SCIENTIFIC ABSTRACT STANYUKOVICH, A.V. - STANYUKOVICH, K.P.

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• Collection: Scientific Abstracts
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• Publication Date: December 31, 1967
• Content Type: SCIENTIFIC ABSTRACT

C3
81907
S/126/6o/oio/ol/012/019
eU_0 0 Elll/E335
AUTHORS-, Stanyukovich. A.V. and Pivnik, Ye.M.
TITLE, Devc,__1,m,_nt of Intercrystalline Fracturepat High
Temperatures and the Plasticity of Steel
PERIODICAL- Fizlka metallov 1 metallove@kiye, 1960, Vol.10,
No. 1, pp lo6 - n6
TEXT: The authors describe their work on different metals
tested under conditions where intercrystalline fracture predom-
inates. An attempt has been made to differentiate between its
various forms and establish a relation between the extent to
which it occurs and plasticity. Tests were made at constant
deformation speeds. as describedpreviously by Stanyukovichand
N.D. Zaytser (Ref 6). Type EI164pearlitic and two aus tenitic
steels were used. The latter were E161211(iron-chromiUm-nickel,
with tungsten and titaniuln) and alloy A (high-strength nickel-
chromium base, with molybdenum, tungsten, aluminium and
titanium). All specimens were subjected to standard heat
treatment (Table 1). Test tempeEatures were 450-8oo Oc.
speeds 180, 3.6, 0.4 and 4 x 10- %/hour. Polished sections of
fracture regxons were prepared and etched. The number and
Card 1/3

81907
Development of Intererystalline
and the Plasticity of Steel
S/126/6o/oio/01/012/019
EIII/E335
Fracture at High Temperatures
overall length of cracks per unit surface were determined and
relative elongation and true resistance -to fracture were also
found. Microstructuresltbtained under various conditions are
shoim in Figs. 1, 3 and-6. Relative elong&tion and number
and extent of microcracks as functions of temperature for types
E110 and B1612 are shown in Figs. 3 and 5, respectively, for
various deformation speeds while Fig. 4 gives the number and
&xtent of microcracks as a function of cbformation speed for
EIlO steel. For alloy A the me-shanical-property results for
a constant deformation speed are tabulated (Table 2). Fig. 7
shows the ratio of true resistance to fractuxe.,-tensile strength
as a function of temperature for various deformation speeds.
In all alloys formation of Intercrystalline cracks at h1gh
deformation speeds begins at 450-500 C. The damage from this
cause increases with rising temperature and decreasing defor-
mation speeds. The number, length and shape of cracks depend
on the particular conditions. At maximum test speeds and
Card 2/3 1@

De-velopment of IntercrystallIne
and the Plasticity of Steel
81907
S/136/60/010/01/012/019
EIII/E335
Fracture at High Temperatures
relatively low temperatures pore cracks are formed: when
conditions lead to maximum reduction in plastic properties
thin and long-sharp-ended cracks are formed. High-temperature
plastic properties are directly linked with the extent of
damage by intercrystalline disruption. The length of the
average crack rises, with decreasing speed and increasing
temperature, to a value close to the steel-grain diameter. The
IncrSase In plastic properties at test temperatures over 600 -
0
650 C (for pearliti.c) and 650-700 C (for austenitic) is due
to reduction in the intensity with which intercrystalline cracks
develop. Intercrystall�ne disruption under these conditions is
characterised by the formation of comparatively small thick
blunt-ended cracks. There are 7 figures, 2 tables and 11
references: 4 Soviet, 5 English, I French and I German.
ASSOCIATION- Tsentrallnyy kotloturbinnyy institut-im.
I.I. Polzunova (Central Boiler-Turbine I
im. I. I. Polzunov)
SUBMITTED,@ November 25, 1959
Card 3/3
titute

LIBERMAN, L.Ya., kand. tekhn. nauk; STANYUKOVICH, A.V., kand. tekhn.
nauk,, red.; LEBEDEVA, N.I., rer.-,--PUDMMF=VA, S.I., red.;
GROSMAN, L.A., red.; KOVALISKAYA, I.F., tekha@, red.
(Materials used in the manufacture of power machinery]Mate-
rialy, primeniaemye v energomashirlbstAtoenii. Moskva,
TsINTIMASh. 1961. 181 p. (MIRA 16:4)
(Electric machinery Industry-Equipment and supplies)
(Electric engineering-Materials)

2708 3/1-125/0 /000/007/005/01'.5
D040/DI12
AUTHORSi '47 a iil S t -a p_v71kcv-' c _ril, A.V@
TIT LE T4n,4_--r@-v o@' welded Jotati :Ln aus-.1enitic steel to loca-1
'@- ' I I I I I YL t
. I- _'T a @- tbe seam a, fi--g 'empera4:ures
PERIODI"AL- Av-1-ocnat'ichf1sKaya 3varka, n,:)., 79 19619 46--53
TEXT, @4. ne.-r L-.Ptiiod for eval-uating the tendency of auStenitic-3teei welded
joint.@s -I,.,:. lo:-ai_ tilrle @,@am at high temperatures is desc;ribed. The
-Tethod _-hojon lir,-@itigati:;ns for the reason that- conver-
';as`5@ d:j .17'ev-eal the dargezo-as -ten-
t: u rr,@, ipmmen@- (particularly austenikic
powex, @qu..
-b jr
w@Len tri-ey ar@ su ,acted to high temperatluxas for
-Dzisisi-q _-Lr) rewiiTig with a constant deformation ra4..,.
were out from joirts with wel
'ir, @i --eeve:rser in@Vih-5
11 T@ 'if
(TaIM-5)
j4:Z;C'7 @R='@. A@V. S+,ar-yuko-qich and N.D.
9) 1-959). Tb.e plasticity of -the iv-
of the externaA. fibers in the
t;3.
r thz- !h-%qier. -ippparan,3e. Experiments were

22949
S/125/61/000/007/005/013
Tand -2-toy @-,f -i@Idvd j,-;_-'%-IS z DOAO/D112
-I a, -;00-1100-@@ w---- i I. def c,:: m. tion rates of 20, 0.60 and 0.067% pe:[
ho-ir. al-ng -he grai-n bourdar-Les in thp ba@@e metal, at.
di-@ia--e of a n s- f@!nm th-i- __'Ane; the charactel: of the
'-@raJtv- vua4 exact3y the aamsa.- ir. of w;@Id3 in austenitic@ steel steam
pipz?lir4;@s. Ti.- varied wiqEll.y ac--ord-ing to the grade of
9 an 0, t@i@_ -b-m-
(JI.e. acnording to whether they had been
weldpl s @) t,.') @ cdt,- haat [e-mail]), Fo-:@ aYi6WqT' (!KhlBN9T) at-eel the
mo@t. dangr-;o@ioi range appeared -tc; be 500-70000; similax or-asks
f':'zm'@d4 Ln_@3'0405 (E'. 405 ), 914 -25'7 (E12.57) (E1612) stsels, but at dif-
v
fer@:,-,' temperatixr;_,.3 and afilsr vazying degrees of elongation of the outer
flbe-rs Thm-, apparqnt cai)sp of cracks axe onsets of
failvxe-- ihr- gra.'Ln !-andaric- -211 +hs at the seam affected 'by the
well-I.ng I-at @ Mn@ n OL, j-_JZA;3 lost their deformatio-yi capacitv
when the @es"- empc-::,aturl@ was raissed, but al '-ready after 700-750 0 0 the plasti-
-y AP@.airl in m-:,-st j.,ints. Ar abrupt d:rop of the intercrystalline
k -I aL t-rip Soam ijp;*,@@ _'ieatirig dii-LInIg the vielding had been stated in other In-
v.-:- a a t i o ri s @o The r;bser,rc---! benell-c-.ial effect of austenization may be
a p v-a r -11,;,a f znib m i o s @ o PI - d ef e c, t s and re d.4 s tri
I but on of the
gr a r. boindar-lez. But, aus'enizat:ion
Caz.A 21/'_@

34521
s/659/61/007/000/008/044
D217/D303
AUTHOR: S.1
TITLE: Estimating the deformability of high temperature ma-
terials
SOURCE: Akademiya nauk SSSR. Institut metallurgii. Issledova-
niya po zharoprochnym splavamg v. 7. 19619 78 - 96
TEXT: A method for estimating the deformability of heat-resistant
materials by constant-rate deformation tests is suggested. It was
found that the temperature-dependence of plasticity characteristics
at constant rates of'deformation when plotted within semi-logarith-
mic coordinatesp is described by a V-shaped curve. Decreasing the
rate of deformation displaces this curve in the direction of lower
temperatures. With the help of a family of V-shaped curves, obtain-
ing by testing a series of specimens and using several constants,
the dependence of the minimum deformability of steel on temperature
can be found. The minimum deformability increases with increase ir
temperature. The relationship between percentage elongation and ra-
Card 1/3

S/659/61/007/000/008/044
Estimating the deformability of D217/D303
te of deformation at constant temperature follows a discontinuous
function until the minimum deformation is attained. Having reached
the level of minimum plasticity, a further decrease in the rate of
deformation raises the percentage elongation. The degree of decrea-
se in plasticity on fracturingg with a decrease in the rate of de-
formation, increases with rise in temperature up to a certain limit
and then decreases again. Deformability increases at the maximum
testing temperatures. Increase in temperature displaces the brittle
range in the direction of high rates of deformation. The decrease
in plasticity of steels at high temperatures is due to intercrystal-
line destruction. The total number of cracks per unit surface area
of the section and the length of these cracks increases with a rise
in temperature or a decrease in the rate of deformation. At a con-
stant rate of deformation, the proportion of intercrystalline de-
struction increasest and the plastic properties decrease up to a
certain temperature limit, the critical temperature. The latter is
higher for greater rates of deformation. At temperatures above the
critical, the proportion of intercrystalline destruction decreases
simultaneously with the increase in plastic properties, and the
cracks change their appearanceg their sharp ends becoming blunt. Rie
Card 2/31

STANYUKOVICH, A.V., kand.tekhn.naukj LEVIN, Ye.Ye.,, kand.tekhn.nauk
Causes of the deterioration of steam superheaters made from
1MN12t steel. Energomashinostroenie 7 no.10:27-30 0 !61.
(IURA 1440)
(Steel, Heat resistant-Brittleness)
(Steampipes-Testizig)

-ZEAZIN, V.N.; STANYUKOVICH, AN.
Tendency of welded joints in austenite steels toward local rupture
under the effect of high temperatures. Avtom.avar. 14 no.746"53
J1 161. (KMA 14:7)
1. TSentraltnyy nauchno-issledovatellskiy kotloturbinnyy institut
im. I.I.Polzunova.
(Steel-Welding) (Welding-Defects)

A,,11, lcand.teklin.llaUk
Anisotropy of t*@-e plasticity of KILU8119Tt s',eel at high temp-oratureo.
Metalloved. i taira. obr. mot. nc.7:57-63 Jl t62. (MIkk 15:6)
1. TSentralInyy nauchno-issledovatel!,@,kiy kotloturbinnyy
institut imeni. I.I. Polzunova.
(Chromium-nickel steel.--Testing)
(Metals at high temperatures)

S/650/62/008/000/024/028
1048/1248
rlO-.-?: "Stanyulcovich, A.V.
AUT'
TITLE: Examples of the application of constant-strain-rate tests
for the evaluation of the performance of refractory
materials
SOURCE: tkademiyp. nauk SSSR. 'Institut metallurgit, Issledovaniya
po zzharoprochnyn splavam. v.S..1962. 184-192
TEXT! Tests at R constant strain rate combined with microstructural
examination of the fracture surfaca, related the plasticity of re-
frnetory materials with temperature to evaluate their performanee
under working conditions. 7/el-ded austenitic steel tubes were sub-
jected to bend tests at 500-90000 the strain rates being 6.7xlo-2
6.7xlO-l, and 20%/hr. In most cases the first cracks appeared with-
in the arcs adjacent to the weld. The plasticityof steels DIA 612
@Ei 612) and _-) ',,114 (,, 4 @ -(EI 405) decreased sharply with Increasing
temperature within the range studied; the plasticity of steel
Card 1/3

S/659/62/008/000/024/028
1048/1248
ExamplGs of the applieRtion...
depth of thread; the elongation decreased with strain rate, due to
intercrystalline failure rat the lower strain rates. The threads
are meakened by defects at the grain boundaries, and by the generat-
ion of local 3tresses during the threading. There are 4 figuresi
Card 3/3

S/032/62/028/011/010/015
B104/B102
AUTHORSt Stanyukovich, A. V., and Chizhik, A. A.
TITLE: Test of specimens with spiral grooves at high temperatures
PERIODICALz Zavodskaya laboratoriyal Y. 28, z1o. 11, 1962, 1361 - 1367
TEXT: It is suggested that the s@naitivity of h@eat-resisting C-r-Ni-Mo
alloys to stress concentrators may be estimated by determining and com-
paring the relative elongations 6 T of smooth specimens and of specimens
having two spiral grooves (Fig. 1), stretched at constant rates (313, 0-8t
and 8-10 -2 @;/hr) until cracics appear, and Vy det ermining the elongation
up to the moment when fracture occurs under constant load. With this
p
in view, experiments were carried out at iemperatures between 500 and
10000C. It was found that, when the rate of deformation is reduced? the
reduction in deformability attributable to the presence of a spiral
groove, is similar to the reduction occasioned in smooth specimens by
variations in the plasticity of the material under test: i.e., cracking
is hastened as deformation is slowed. Plasticity diagrams (Fig. 5) reveal
Card 1/0 -7,

STANYUKOVICH, A.V.
Investigating the effect of stress concentration on the deformability of
heat-resistant alloys. Issl. po zharoproch. splav. 10:93-102 16j.
(MIRA 17:2)

ST,UJYUKOVICH, A.V., kand. tekhn. nauk
Collection of papers No.9 of the Leningrad Yletalworking
Plant (22d Congress of the CJPSU) "Properties of ma-terial#
used in turbine manufacture and methods for testing them"
published by the State Scientific and Technical Publishing
House of Literature on Machinery. Energomashinostroenie 10
no.2:48 F 164. (MIRA 17:6)
0

2-56 i-MV 2IL,-IP I! V'_-, '&g(tjy&T --Lc) a,
@___!j
ACC NRI AR6oww(3o SOURCE CODE; UR/O124/65/0OO/009/VO78/V0P
.P
AUT'HOPS: S@tanyukovich, A. V.; Nikitin, V. 1. 41
TITLE: Evaluation of fl&igue resistance of steels .n elastic-plastic regions at high
temperature
SOURCE: Ref. zh. Mekhanika, Abs. 9V664
REP SOURCE: Sb. Vopr. mekhan. ustalosti. It., )iTashinostroyeniye, 1964, 220-225
TOPIC TAGS: austenitic steel, fatigue test, fatigue strength, plastic
deformation 0 SrR-995., '0W19e-rVR6 I I
.A3STRACT: The results of experiments are presented on fatigue at high temperature
(7000) and symmetric periodic changes in deformation with low frequencies (20 min
in the elastic-plastic region. Tests were made with rings of uniform deflection
resistance, prepared from three austenitic nickel-chromium steels with differing
yield stresses. The dependence of the logarithm of the numberli3f cycles up to frac-
ture on the logarithm of deformation after a cycle for the various steels is
represented by parallel straight lines. 'With identical amplitudes the general deforma-
tion of the steel with the higher yield stress sustained a larger number of cycles
without fracture. For equal amplitudes plastic deformation of fatigue resistance is
higher for the steels having the lower limit in yield stress. The experiments show
that the longer the material remains unfractured the larger the general plastic
Card 1/2

STANYUKOVICH, A.V.
-, " , - @
Regularities of Ulu-, manifestation of a tendency toward brittle failure
in steel at high and low temperatures. Metalloved. i term. obr. met.
no.7:2-7 Jl 164. (MIRA 17:11)
1. TSentrallnri nauchno-issledovatellskiy i proyektno-konstruktorsk:Ly
kotloturbinnyy institut imeni I.I. Polzunova.

L 21819-66 EPF(n)-2/aiA(h)/z-W(m)/T/~-!,WA(d)/94P(w)/3'IP(t) IJ'-P(e)
ACC NR: AT6008658
" ( rv) SOURCE CODE: UR/0000/65/000/000/0147/0156,
GS
'AUTHORS: Stanyukovich, A. V. (Leningrad); Chizhik, A. A. (Leningrad)
If ORG: --onb-ne
& IA
;TITLE: The effect of various factors on the sensitivity of refractory materials to
istress concentration at high temperatures
SOURCE: Vsesoyuznoye soveshchaniye po voprosam staticheskoy i dinamicheskoy
IpKqc4yLqsti materialov i konstruktsionnykh elementov pri vysokikh
--T
temperaturakh, 3d. Termoprochnostr iWi-erialoi-i konstruktsionnykh ef6ie'n'-i&-(Tfi4iiii1
iitiiRiffi -- of -materials and construction elements); materialy soveehchaniya. Kiev,
Naukova dumkaq 19651 147-156
TOPIC TAGS: stress concentration, high temperature metal, steeli alloy, pearlite
steel, austenite steelq chromium steel/ B1602 chromium steel, 1Kh18NqT chromium
1 steel
i ABSTRACT: The effect of the cut geometry, temperature, and rigidity of stressed
state on the sensitivity of refractory materia s to stress concentration is studiedoll
!Specimens with a spiral cut were tested (see Fig. 1). e testing method and
ISard . 1/3

L 21819-66 -------
ACC NR: AT6008658
rad
Fig. 1. Specimen with
a spiral cut. r
WO - x I#j4W _.V
the auth d k
certain similar results were published earlier b3T( (z 81a
laboratoriya, 1962, No. 11). Samples of 12'KhlMF, 1Kh18NqTI EIiomm 2@and EI604
steels and Cr-Ni-Co and Fe-Cr-Ni-Mn lloys were tested at temperatures to 12001
(see Pig. 2T--i'rI-,,1 -VI
Fig. 2. Change of the coefficient of
sensitivity to spiral cut with respect
4
to plasticity IqP as a function of 42
temperature: 1 Z 12KhIMF; 2 - 1KhI8NqT;
3 - Cr-Ni-Co; 4 - EIIO; 5 - E1612; 6
EI802; 7 - Fe-Cr-Ni-Mn; 8 - lKhl8N-gT-
18@ cold-hardened. AW
9 V

L 21819-66
AC(; NR: AT6oo8658
@The pearlite steels showed high deformability at 823K. Chromium steel E1802 has
greater workability than 1Kh18NqTf which is less plastic at high temperatures, The
high-strength austenite steels showed an especially sharp reduction in plasticity
.with intercrystalline breakdown and the action of a concentrator. Orig. art. hsss@
i4 formulas, 5 graphs, 1 diagram, and 1 table.
@SUB CODE: 20, 11/ MM DATE. 19Aug65/ ORIG REF: 006
-card-3/3-

ACC M AT7006337- 66DEj 11
AUTHOR: Stanyukovich, A. V. (Dootor of technical soiences)
ORG: non'e
TITLE: The influence of grain size on the deformation abi?.ity of pearlite steel
25KUW (EI10)
SOURCE: Leningrad. Tsentral'W nauch-no-iseledovatellskiy i proyaktno-konstruktorskiy
kotloturbinnyy 4natitut. Trudy, no. 69, 1966. Iseledovaniye materialov dlya
energeticheskikh ustanovok (Investigation of materials for power plants), 109-118
TOPIC TAGS; metallurgic research, steel, pearlite steel, metal teat/ 25KhW steelt
',',110 ateel
ABSTRACT: The effect of grain size on the long-term stability and deformability of
steel 2 V
@Will& (EI10) was investigated. The 'Mvestigation was undertaken to determine
the cause for the failure of a number of steel boiler collars used in the
Pridenprovsk GRES. The investigation supplements the results obtained by A. M.
Parshin and Yu. V. Kolosov (Trudy LPI im It. I. Kalinina, Mashinostroyeniye, Yashgizp
1961). The mechanical proper-ties and microstructure were investigated for collars
-ff;,'.h diameters of 36 mm, length of 770-1600 mm, and curvature radius of 185-210
Tho experimental results are summarized In graphs and tables (see Fig. 1). it was
found that plastlic deformation suffered by the outer fibers of the collar may be
Card

ACC .1"' Ri Ar,170063 37
140
@@x h
C"JI /00
Fig. 1. Change in the true str
ength i 649
06
of steel 25XhI (EI10) with coarse-
grained structure as a function of 40
4.
%lemperatureo V.- %..deformation per
how 20
0, L
X0 -,go 5W WO 7XI
represented by the eqi@ation
Card P A

ACC NRt
AT7006337
where A is the diameter of the rod, and R and R are the raditts-of curvature before
1 2
and after uset respectively. It is concluded that the presence of coarse-grained
structure lowers the impact viscosity of the steel and leads to a sharp increase in
the tendenoy to brittleness. Orig. art. has, 3 tablest 7 graphs, and 1 equation*
SUB CODEz 11/ SUBU,D&M none/ ORIG REP: 008/ OM REFt 001
Card 3/3
t

STAIFYUKOVICH, K. P.
"Application of Certain Empirical Relations to the Study of Meteors."
Astronomicheskiy zhurnal Vol 10, No. 4, 1933, pages 457-463.
Translation 563974

-r I'T 7
Astron. Zhur-j Vol.
Fesults of tkhe Fhotographic Stludy of a Bright l4eteor
12, No. 5(1935), pp. 44,C-41i(i

STIVITMOVICHY K. P. and Pokrovskiy, G, 1,
"Elements of a Direcyed Blast-," report given at the General Assemblies of the CFWi
in 10,44. Iz. ARad. Nauk-, STer. Pit., Vol. IX, No. 3, 1945

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00 a whaim 11I- Fmioudy
go Acat Xd- umd to mudy the
(ma, I. ---.
00 priceum 41111111" MIII ...... WNW, tim a
Ick I G"Oft zzw- or twm
a
NCT&LLUROSCAL LITCOAV461 CLASIVOCAVION
DO
U ON A V As
00 0000 00 000 0 0 e 0
'00
-Of
1-00
.00
.00
see
L
eel
'A 411
as 46
oil
W-T--Sv ado 0 *-IV asne

:. i';', - -'r. " :;,@ : - -
I j... - , - .., 1, . rl.
III-,".- ti-le i@eflection of a Det-juati Lave ironlu-,," Com-Aes Aendus (Dolalady), Jol 52,
I@o C -9 6
. -L 4

if if 1, It ta tj a It a 4 JI A a J7 a
-1, --k- W.
A I-T- --i- -L -A
--fur !@m7 .... ...-
P"PINTIEW
00

Determinatim of the exponent in the retationsbip de.
ibi
th
f d
d

'00 scr
is ststos o
eema
ng
ect products. G. 1. Pokrov-
skit atilt K. P. Is. Compt. FfXj. arad. J'i.
WRU-C
-
U.R.S.S
11 V
93
Landau
C
A
4
W

00 '
.
.
.
-
.
,
,
.
Pfw Products fwmed by a detmation of local-action ex.
1
i
ffi
f
i
d
4)%
vt:s o
su
c
ent
j?
.. the law of adiabatic expansion is
** A ft*-conit. The exponent was detti. by tucamring the
00 # angle insute by the direction of max. ti. of the energy flux
aii-I nimuentum flust its the explosion products, with the
di
l
h
h
i
C
'00 cu
Perpen
ar to t
e c
s.
arge ax
urvtd charges were
ct oft a At plates, and x was found to be 2.85 a 0.13
*0 for a Use with tdryl eme. and 3.D - 0.5 for TNT charjrc@,.

0 The intemal radius of curvature of the charge was vaded
between 2.5 and I I cut. without effect on the distance.
Ern-t Af. Cohn

@

Z
of J*C r m
q
2X
age
see
ass
1,171MAURE CLASSIFICAVOR
St A FTALLUAMOCAL
--7
---flilil --AK-.---T%t
tv 0 IF a 9 a a :P
T I . I F
I i IA
U U Im 43 is' I't go Is X 4 19 W 't it tt is Ot KW P '14 000000000 so 0
0 1,00 * 0 0 000 so so* so 0 0 a 0 0 000000
66 000
0 0 0 0-0-9-- 0 SAAMIA -0 Ob

egg* di 48 Imcumd, 40044" ww*" (in IAalffth), V. R.
'jM4..Vri, URSS. F44-. 10, 1647, Vol. &I, W1, 4, pit. all. 3M
Ttv p%m froat eta de4ameAm wave Is ommml to wAv Aw4g
oo plam bamAmy of a abarr. the ON* a betwom Own two
I J-4 C
4/07
pbwo I ' &@ ownwaL TW wAbw wpwndy ovAmw a
'Wr burshms of St go @ n" m the wave in a
q4m w4vft with an wove, 110 I%w d as 4ANWIM predwis
ojotanvom tdV of the dwoW IMb " is euvied mA mWw
tho Wo"-fitiou oat C, - Dolto + 1). when C@ IN the Initial volve-
Ity of ""Ime, 1) Is mppwmuy do %leAvounn vTlmty, 04 a
I'/-
Curvm Aawks the amoder diAdbutiou of the #new of On
*60416aft p -1 we I , for so @ * - 45" go* teb.
pthe with m 3.4. &Q. SmA of dom *Awe a dorp pmah, at a
&rtmin amoo of bwA-v=Uoft w" I -, I on a and oL
(;Wd - - W ewnwa oft expWisma" wmeb "m nab
tnwWlyforthopurpow. 7W&pmpwk&NkmftIorrAdl - i
ftMAtk" we not WORGIMOY fqA%hWIi in.Kur4fJ,ITI4A

'
ie 0 0 0 0 0 * a a 0 0 0 * 0 0 0 W-W
6 0 0 0 0 0 6 0 0 0 IN a 6 a * 0
I
Oct,
f
l
.
a m a k m x It a 44-
I
i "" @-A!
A A L a -1
11 v
a a r a a .1 -1
l
m 0
-
i
I
0

00 @-00
-00
00 -00
00 c
-
00
0* 00
00
00

04, IWO.
an 110@
-00
vwK ) 9, AM
I
" e4
asee
w tok
URM
112@1 Ot low =00
ba ellilk"
d
W
aid
do VdIft
do
71 see
00
an dWhW see

o

00 G-T- . VIDIS

00 ;;99

40*
Moil

asm@SLA NtTALL.4111141CAL LITINATUIllf CIASSWKATIOU No*
1143M 44WIRW
4I&LA71 amw Aft
'

b u a IT vo t F q 11 rFA a It a a a 3 4 111,
11,
.f It w "a Is
0 Owe*
0 0 0 0 0
e
0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 4 0 0 * o a 0 a 0 a- 0 a e s
a

'3
T IPovio' IAYOV BORI-SOVICH, and K. P. SWJIjLIK(;.TCfj.
IYU --. .. --
Ob otra7henii ploskoi dr-tonatsionnoi volny. (Akademiia Nauk SSSR. Poklady.
"ovaia seriia, 19147, v-55, no. 7, p. 591-594, diafrrs.@
Title tr.: On the reflect",m of a plane detonation wave.
Also Dublished in English in Comptes rendus de l'Acad&nie des Sciences
de 11i7RSS. Noi:.velle s,@rie, 1947, v.55, no-7, P. 567-590 (Qu'O.A52i
AS262-S3663 v-55
SO: Aerorautical -Sciences and Aviation in the Soviet Union, Li1brary of
r, Cf
von,@-ress, 1.0-115.

T-t-i iq J I
Jul 1947
Astronomy
"Destructive Action of Meteorite Blove, K. P. Stan-
;@4qy@qh,, V. V. FedynBkiy, 4 pp
"Dok AJm& Nauk SSSRS, Nova Ser" Vol LVIII No 2
larger planets of the solar system are subjected to
constant bombardment by meteorites that hit planets
at terrifiC speeds and result in a slight destructive
action. Presents formulas for calculating destructive
action of meteorites hitting earth. Sulaitted by
Academician N. N. Semenov., 14 may 1947.
60T102

Ast 30T
aim rum
Gas Pressim
w2woI-%* Discharge or a Qku frcs Cylindrical a
Uto Pipe K. P. Stanyukorloh, kpp.
036k Akad Awk OMP Nova OWN Val LVIU, So 2
D"evisses me oUnwe froquent-ly Ifts In the,
flex of gas dynamic w: vhva@,& pw is disowe"'trem
orlIzArical container or Isnaft I into pipe InAoft
dimtlans, fty is itthat theAlsokargo does.act
teglul'-sisultanscusly?, IM PrIMU7 state'the vis'le
pissive, but'its @ prosev"i wA denaltr constant Pr*-
showum reasons for this phMassaft. at
@M/ftaics (Coutd) "I"T
@vsu flow of gas rroa acutaluer to. pipe. ftbdtted
'by'Aaadvaiclan K.,V. X614yeb, 5.Apr 1947.
rA

SrfwfuKoVic@fl
*movement of a Particli of the Products
of a Linear Charge." K. P. Atw9mi-C-40
."Dok Ak Naukm V01 LVIII, No 5
of Detonation
Wch intereat ia shovn In the stxWj of particles of
the products of detonation of any charge after':the 00-
currenoe in it of detonation waves as well as during
Its dispersion. Author discusses methods whereby it
is possible to determine simply and with a fair de&ee
of accuracy the movement of partioles of products of
detonation In cloaa proximity to the actual explo Ision.
Submitted by Acedemiclan N. N. Semano#, 4 *Y-119
38T100
Chargeill- . .....
Detonation Wrects

0;0 0 0 0 0 a 0 0 0 0 0 a 6 0 0 0 0 e 6 , * , P z @ -1
4 6 G 0
ez; t r 4 1 so if u Ij u is m it so " A it a, n b a IS 11 b M JO 11 U U 14 U M 9 N 419 At At U
A f F r IS I L-J--A-X-?- 9 R .1 A-IL 1: 11 QD U b
533A011 - 533.7
so a 2Y". %vW MkOM af So Sm*4%vmdr
00 a OVWdSM fW OMW VJMMWk 009M SWVAMVKC?-,
vK". K. P. DML AmL MM,
11414OW hr Akuhulf-The ft fm
danges or crAnW. Aftr mmA oWim Wvs-
0* Fm ti@ da symm PI '10 1*' sm* Whole.
fur"Ming Wkwoms of a MW dm at "Mmemliw, zoo
Oe nwfivm of Ow ps wbkb we I g p Ibr swo-
044 physic** I Al - 'Seff-doft ar"Iftemb we
Akfmed a WAvemnib the - 0 of Am
Wn O"T F -- in OW L
In dim. TV* 'we dom to bc
00 &1 FRbsev-skmilar Note" skew? F, - I -
in specud caw& by odier mg1bods. AmomS the
ev=Wk$ UCUW is the mas arms manxim of pl@
9mck wava of varlabb WWW. 'I$ V a OwAmt
W10city. IL F. K.
bee
ALSIP.$ A G&TALLURSICAL LITINATURf CLASSWICATIOM
-77
.Alt $4j;O ,vjWgIj 9 1 11 1
0 0 04 0 0 0 0 0 0 0 0 0 4 0 0 0 4 0 0 0 a 0 0 a 0 0 0 0

USSR/Physics-.. Jill 48
Astronon*r
Mathematics, Applied
"The Problem of Angular Moment of Momentum of
Planets in the Solar Syi;tem,:.L @- St@a @4@
3 3/4 pp
"Dok Ak Nauk SSSR" Vol IXI, No 2
Explains significance of subject for cosmogony
theories. Obtains equatio n for nass of gas thrown,
from a cylinder of uniform section. Eraluates this
equation and applies result to case of gas thrown
out from a star. Submitted 10 May 48.
11/49T98

", -
It 'f, lact-@cs),
Staj,rrukovich rK. anA FedynsldY, V. - "!;-I tile spaces Of tile UnIverse.1 k -12
m y bDilshevJLk, 1-14L.9, N0. 7, p.62-69, - i@i-)Iiog: 6 itepis -
.0
So: U-3736, 21 i@!a,-,, 53, (Letopis 'Zhurnal nyidi Statev, L--'io. 17, 1949)-

steady Wpt@An Cf a za Doklady Akad. Nauk SSSRI@*
fi of-
The author- t eats fami tes of, steady 6 a t@rii
del specifi
sible fl.uid which fall, under his automc
A flow, is tei med "autoftxle)" it ihe solution depends esien
tially upon 'a suitably cl@mcn single independ
ent parameter
which'is it-,;elf a funct:on of the originally specified inde@
pendent viriables@. In tlc cases investigated the restdctiaf@,.,
-i-syrnrriet;ic fl %v is made at the outset- No
to plane or u 0
:a priori specification i5 made asA1-1 irrotationality or Isim-
tropy. Prandt]@Meyerflowand the conical flow of Busemannt
[Z; Angew. INIath. 111c.01. 9,49"98 (1929)] are obtained[
-ne riore general solutions are obtainedl.,
as, special cases., So.
in the form of unsolv(d differential equations. Fi all it
In 19
Ows
r the most general case of steady spatial (I
noted that fo
o find a-it6modelsolutions h d
it is impossible t -whic ern on
only one parameter. W. D. Maya (Priividence@,.P_ 1.)._:
4
10'.
Souici@s 'Mathematical-Reviews, 'Vol 0.

STAII@KGYF@
]p d Me c A I c- -1
gas (its RivAim), Mh-littlyll kad. Nauk .14'.4hilt 111, 467 A70 (Feb..
71 _15)
riv, viluitumit forepherit!al waveli W a coisilimr4blL poll&,'rabl"
me'llitiol lift) %klittelf In the form
r" I rl(u, + it if, + pr1p I, + 4-m(op
(tog p), + if (lug p), + it, + 2u/r - 0,
(log p), + lf(log p), + Of, + 2,t/),) - 0,
wbeto p k lift, pr(-n,-mrv, if iltmhity, it radial "locity, 6 lift, gravi-
tatioluil cowdnnt, find k file mtW of.-ipocilit; bvituj. Tho I'vilow-,
big of "Ittilliniollul 11i'viums" (correspontling to &-dult
vAllvil "Imgiv.4.@itig wnw,)" its C"11111fil. 111141 Friedrich'zi Stept r-
isoltic Poll; find Shock Il'ifu-1, New York, 191S) im, inviNtigilvil:
x r1l; p - up rill% artial Eliffercidial vimatiou.
P, s fire
obtained for x, y and p; them are trajisformed III(,) ordillarv flif-
ferefitial eijtmtiom@ byassuaiting thid r, y aml il - p12 life functions
'if the @Suvlc varitible z - rt -1. The alm-eial vivei z - r nm
considered.
(2) it = r1t. It Li found that p mid A litcome of [lie form
A r-10, svilli certain rdatium, bkAWETR OW k@Xjlllllellts Alld the
factors A.
(3) u - 0. It follows that p and p are funtAitmi of r only.
This leads to no equation of Eitideits type for ga@vous, plivi ej.
(4) xr; p - ypri'. A solution 14 smight III which r, yand p
Lire function.' of the 1.411gle variftIAL z - re-,,.
Al. 11 nrgvr@?, Ifullaiscl

'A - !,
--J I K. - r
JK
USM/Physics Feb 49
Gas Flow
Mathematics, Applied
"Conformal Motion of Gas In a Gravitational Field,"
K. P. Stanyukovich, 4 pp
"Dok Ak Nauk SSSH" Vol IXIV, No 4
Mathematical treatment of various types of Conformal
mWon In gases with allowance for its own inner
gravitational field. Sabmitted 6 Dec 48.
27/49T101,1

'A
V
USSR/Physics - Jon 49
Gas Flov
MatherAtica, Applied
"Conformal Surfaces and Axisymmetricil Steady-
State Flow of Gas.," K. P. Stanyukovlch, 3 PP
-Dok Ak Nauk SSSR- Vol LXIV., No 2
Strict mathematical treatment of subject. Sub-
mitted 10 Nov 48.
25A9w

STAITYUKOVICH., K. P.
"Elements of the Physical Theory of Meteors and Crater-Forming Meteorites,"
Ak. Nauk SSSR Meteoritika, No.7, 195o
Translation 56340---

USSR/Astroacm Cowcanw, 601W Systdo YAW1Jv& 52
"Problem of Origin of the Solar System," C. P.
Stanyukovich
"As tron Zhur" Vol XXIX, No 3, pp 288-306
Author above in his computations that the solar
1=59 should have been 5-15 times greater and also
its angular velocity 5-1@ times higher in order to
erupt,gemes in sufficient quantity for further
formtIon of planets. In the case, of such initial
conditions, only 1/100 of the escaping gases
217T49
exVanding in the direction of solar rotation will
revolve m elliptic orbits, the remainder
necessarily falling back on the sun. Received
li Doc @1.
217T49

USEPR/Astronomy Astronomers Jul/Aug 52:
"Fourth Plenum of the Commission on Comets ard
Meteors and the Commission on Planetoids of
the Antrorr7mical Council of the Academy of Sci-
ences USSh.11 K. Stanuykovich, V. Fedzynskiy
"Astron Zhur" Vol 29, No 4, PP 505-508
A meeting of the Commission on Comets and Me-
teors and the Commission on Asteroids was held
6 - 8 Dee. -51 in Kiev. Thirty representatives
of astronomical observatories attended. Prof
V. V. Fedynskiy, Pres, Commission on Comets and
226T48
Meteors, opened the session. The main subject
was S. K. Vsekhsvyatskiy Is theory on the orig#
of comets as eruptions from planets. Ilia theory
met strong criticism.
226T48

2. USSR (600)
4. Astronomy - Congresses
7. Fourth plenum of the Committee on Comets and Meteors and of a committee on minor
planets. Astron. tsir. no. 127, 1952.
9. Monthly List of Russian Accessions, Library of Congress, May -1953. Unclassified,

STAWIUKOVIO, K. T
Among the papers presented by tht) First All-Union Conference on
Aerohydro@lyna,nics (8-13 Dec 19c@2) ccnv;!r-ed by th,_@ Institu'V,@ of
Machanics, Acadf.,rny of U3,M, waF@l
11132sic Mechanism of the Motion of a Gas in the Field of Gravity" by Stanyukovich,K. P.
(Institute of Physical Problems, Academy of Sciences USSR)
SO: Izvestiya AN USSR, Otdeleniye Tekhnicheskikh Nauk, No. 6, Moscow,
June Z53, kw-juboe, J_e dulY IY54)

STANYUKOVICH, K.P.
"R
Nov method of approximtion for the integration of certain equations
of the hyperbolic type. JDA1. AN SSSR 93 no.6:979-962 D 153, (NLRA 6:12)
I.Tredstavleno akadealkon X.VeXeldvahes.
(Integrals) (Differential equations, Partial)

STANYUKOVICH., K.F. Prof. Dr. Tech. Sci.
"E'roblemy m-ezhq:1anetnyI--r1 polet" (Problems of' interilanetary fl�ghts),
Krasnaya Zvezda, August 10, lq.@4
.p p.
For translation, see Appendia VII,
OOL 5 -V
('A

STAITYUKOVICH, K.P.
'Taketa i ee budushchea" (7he rocket and its future),
Krasnay;u Zvezda, December 19, 1954, P. 3.
A review of the book Raketa by B. V. Iya-Dunov.

STANYUKOVICH, Kirill* P. Dr. Tech. Set.
"Trip to the Moon: Fantasy and Reality," A Soviet Review of World Events,
No.n. pp. 28-290 1 Jun 1954
In English

Problem of the origin of meteorites (thesas of a report). Ketec-
ritika no.1-1:63 154. (MLRA 8:3)
(Meteorites)

STANYUKOVICH, I.P.. doktor taklmicheakikh uauk.
IThe nature of gravity. Nauka i shisn' 21 no.l."21-23 Ja 154. (ML" 7.'1)
(Gravity)

8TM1VLtKOVTC;T@ X,P,
VARVAROV, N.A.; DOBRONRAVOV, V.V.. professor, doktor fisiko-matematichs-
*ikh nauk; )VMUW14V, I.A., inzher,*t-konstruktor; SARTAPIN, A.D.,
laureat Stalinakoy premii; STANYUKOVICH X.P.. professor, doktor
takkinichaskikh nauk-, KHLZVTdWM':"'!iu. didat takhnichookikh
nauk; SHTERNMID, A.A., laureat mazhdunarodnoy pooshchritollnoy
premii po astronavtike.
&route to the stars. Tekh.mol. 22 no.7:1-7 JI 54.
1. Predsedatell maktaii astronavtiki pri TSentrallnon aeroklube SSSR
imeni Chkaloya (for V4rvarov). 2. Zamstitell predsedat-slia nauchno-
tekhnicheskogo komiteta po koemichask6y navigatsii, sektaiis-astro-
navtiki (for Dobroaravov). 3. Predsedatel' nauchno-tekhnichemkogo ko-
miteta po raketnoy takhnike, saktotia astronaytiki (for Nerkulov).
4. Predsedatell nauchno-takhnichaskogo komiteta po biologli kossidws-
kogo poleta, sektaiia astronaytiki (for Seryapin). 5. Chlen nauchno-
tekhnichaskogo komiteta po astronomicheskim i fixicheskim probls@
(for Stanyukovich), sektaiia, astronnytiki.6. Predsedstell nauchno-takh-
nicheskogo komiteta po radio-teleupravleniyu (for Kh1ebteevIch), ask-
taiia antronavtiki. 7. Predsedatell nauchno-tekhnicheakago komitets
po kosmicheskoy navigataii (for Shternfel'd), sekt9iia astronaytiki.
(Interplanetary voyages) (Space ships) (MLRA 7:6)

STANTUIOVICH, K.Pdoktor tekhnichoskikh nsuk.
1---, -1-1--. -
The nature af gravity. Tekh.mol. 22 no.12:3-7 D 154.(K6U 8:1)
(Gravity)

STAIMMOVICH, K. P.
"Silov-je polya" (Fields of Force), Tekhnika-Molodezhi
Vol. 222., No. 12, December, 1954, p. d.

2425. Stanyukovich, K,.P., (kneral solutions of tha@ eq4jL-
tioua of giti'@am 4Wr one-dimensional motions for a cwtils
Clion. equation of Otsta'ar procesi (In Russian), Dakk4i Akad.
U S S R jv--h 3M Ovs.) 96,441-"4,1054.
Cozialder ant-dimenfilonal nanateady f1o* With
And lot (r + -ra) (h + Aq) (v + vi)pj whero It premMej
V speciflo volume. A - h(a) otam of the I" buluinn. from x
to M, a entropy, ILY, an arbitrary functfun of h, while k, A. 4 and
ra ara constants. Side& the Lagrangian lbtrn of the equatlant of
Imotion irnpli.en alz/br' deflu to by
bio"al + -0, btv/ar + .4 HPAbz/al i.. 1) ("1
If J - 6(W, A)ligl, 7) 0 0, traneforat t *165- thwaitig tD 9
Indopentlent, t, r is
w
re a U/(k - 1), and let k - (2n + 3)/(2A4- 0 11er n-
b e
Then t(8, W) eat4fies'a Wel-DdAdtix equa-
tion whoee general solution in terms of derlvatl*i of LWD arbi-
t rary funcUona of 0 zl-- to is k nown, and r cin be fauhd bY a q, tada-
ture. Mier iuversion to obtain Z(1, Tit the putliclt' jjy can
also be folind by a qwArature. The (6mplo waje) " e -0
in molved in a form involving an vbitmty flinction xr(z)- The
author suygests that by proper vhoir;i of A, )% aid ort(h). flows of
this t@p-i rittky be iv@ed to approxinuito flowzi with shookf'-
J. n. mew, Usk

BRONSHTJW, V.A; STANYUKOVICH K.P. doktor takhnicheakikh nauk, redaktor;
' - 0
[e-mail]'., ';e d@akto'r.
[The universe; a collection] Vselennsia; sbornik. Moskva, Goa.
izd-vo kuliturno-prosvetitellnoi lit-ry. 1955. 404 p. (KM 9:4)
(Cosmology)

ST"THOVICH) Kirill Petrovich
Unsteady Notion of Continuous I'ledia.
745 p.
Translated from the original Russian:
ZI
Sploshnoy Sredy. Moscmz, 1955.
Bibliography: p. 738-710.
New York, London, Perg-amon Press, 1960.
Neustanoviv sl-!,Yesya Dvizheniya

VKOYIC
Motion of a a
conthwom irwillum.) Gosudarstv, lid t 4$4
-Teor. 1, t., lffo,,@ o t1955 804 pp. 26.35 rubles: IJ
I of a
@njisi is an exhaw;the trcati@e on unsteady motior
;atJgis witb particular application to the theory
'al
R @losions and tointernal 'ballistics. Much maten is
assenibled which has pieviously been widely scattered in
reWarch publications and, in ti-an-lated form, would be:
of gre@t value to Workers in't h, explosivei fi6ld; Sibce, at
present, ther#,_ is no-.equiv-dent book written in Englisb..
Th * f' t hapt@rs- deal with -Ahermodynami
e 114 wo c
_jranzep&1mid the* fundanienW equations of motion, in-
T'
cluding jw uccoimt- of the method of characteristics.
-of
CliapW III is conceravd. @k4tll self 'similAr motions
i media and cotitains much new material due to Sedov and
his. group, Chapter III &scribes special solutions for
isantr6pic -flow. corresponding to y=3 and other simple...
6nal'isentropic
gas kws. Chaptex V treats ane dimensi
motion, especially probleqLc of intemction of rarefaction
waves. The three faflowing chapters deal very tfibroughl@
-With-th detonation waves. i
C -Ae_ ecount-, -pro aga.,o
x
md

SOV/124-57-5-5264
Translation from: Referativnyy zhurnal. Mekhanika, 1957, Nr 5, p 22 (USSR).
AUTHORS: Baum. F. A., Vsekhsvyatslkiy, S. K., Stanyukovich, K. P.
TITLE: On the Explosive Processes of Power1_u1_V`oT_c_an-i-c-ZYUpttM (0
vzryvnykh protsessakh pri moshchnykh@ vulkanicheskikh izverzheni-
yakh) in Ukrainian
PERIODICAL: Nauk. zap. Kiyvslk. un-t, 1955, Vol 13, Nr 7, pp IZ3-130
ABSTRACT: The paper analyzes the question of the sources of energy of the
gigantic explosive processes observed on numerous occasions
during extremely powerful volcanic eruptions (Vesuvil.s, Fujiyama,
I'Sangayll,"Papandayang", Osamayama, Tamboro, "Gunung-
Gelungung", "Kazegvinall, Krakatau). It is shown that'utider condi-
tions which exist at extreme depths of the earth there are accumu-
lated tremendous quantities of H2, CO, CH4, etc. At elevated pres-
sures and temperatures these are explosive mixtures high in energy
and readily detonated.'" Various r"r-MMI-Are analyzed and an evalu-
ation of the energy released is made.-The total amount of the energy
of the explosion is calculated which is required to eject solid rocks
Card 112 of several scores of cubic kilometers in size (Krakatau, August 27,

SOV/124-57-5-5264
On the Explosive Processes of Powerful Volcanic Eruptions
1883). It is also shown that the velocities attained by some individual rocks may
exceed 8 km/sec.
From the resumf
Card 2/2

STANMOVIGH, K.P.
I......... .........
DetermInIng,zeteor trojectories in the earth's atmosphere.
BluLTAGO no.16:7-14 '55. WaA 8:6 )
1. Noskovalwye otdolonlye VAGO.
(meteors)
--T@O,,uw I f-G 3 3 @ q

STANr W VIGH, K.P.
@:
Principles of relativistic gas dynanics in magnstic fields. JzV.AN
SSSR Ser.fiz.19 ne.6:639-65o N-D 155. (MM 9:4)
1.Koskavskoa vyssheyo tekhnichooksye uchilishche imeni N.I.Baumana.
(Cosmic rays)(Nuclear physics)

STANYUKOVIGH, X.P., doktor fiziko-matematicheakikh nauk, professor.
A few problems in the elementary theory of gas mixing. [Trudy]
KVTU no.32:5-25 155. (MM 9:8)
(Gas flow) (Diffusion) (J*t propulsion)

-SWYUKOVICH, K.P.. doktor fisiko-matematteheskikh nauk, profwssor.
Calculating the thrust of various jet propulsion engine.s. [Trudy)
KM no.32:26-46 133. (NLRL 9:8)
(Jet propulsion) (Airplanes--Jet propulsion)

SMYUKOVICH, X.P., doktor fislko-matematicheskM vauk, professor.
."-DM4.1
Problems In the tboory of pulse air-jet engines. [2@mArl MM no-32:
143-156 '55. (KM 9:8)
(Jet propulsion) (Airplanse-Jet propulsion)

TA At V K L/ I C, j
USSRI Physics
Card 1/1 Pub. 2.2 - 19A6
Authors S. Stanyukovich, K..
Title Some results in the domain of relativistic magneto-aerodynamic's Igas)
Periodical I Dok. AN SSSR 10311, 73-76, Jul 1, 1955
Abstract t A mathematical analysis of the.aerodynamic expressions for gas movement
and the energy cm@servation in. amagnetic, field, of relativistic domain
(4-dimensional space). -Cases of'one-dimensio 'moVemen are .@wndidqred@
Four USSR references (1947-1954).
Institution The Higher Technical School imeni.Bauman
Presented by: Academician N. N. Bogolyubov, February 16, 1955

OTAITYLEOVICII., K. F,
2'7 K L L
Roc' e@s for interplanctory Tru,.rel, " a chapter fron the book Problens
in -'Ube Uti-lization -of Atomic Enerig, t;ae second revised edition of a collection
of 3rticlles, published in 1956, Moscow, USSR

ZIGSLI, Yeliks YurIyevich;.�WjWjQXLQ#aj4ZU nauchW redaktor,
GOIJJBILOYA. V.A., redaktor; YUSFINA, N.L., tekhnicheokly redaktor
[Can stones fall from the sky?] Mogut li a nebm padatt kamni?
Moskva. Gookulotproevatizdat. 1956. 10 p. and 6 Illue.l.
(He te o ri tee ) (MLRA 10:2)

STANYUKOVICH, Xirill..Petrovich@.doktor takhaichiskikh nauk; MANIYXVA. M..
-1-1-- 'Al -1- -111:--.1,!-, -
redak of; MIMnOVGUTA, K., tekhnichaskly redaktor
[Cosmic flights] 0 koemichaskikh poletakh. [Moskva] 1zd-vo TS1 TIM
OKolodaia gverdita," 1956. 30 P. (MM 9:11)
(Interplanetary voyages)

STANYUKOVICH, K.F.
S79tem of air shock waves during the fall and explosion of meteorites.
Meteoritike no.14:62-69 156o (MIJU 10: 1)
(Meteorites) (Shock waves)

ST.@ UKOVI-CHI
T
.nt@-r
5 no. 12, D'ec. 2' - -
D T : I- .1of, 56.
3C: Yoathl@, li-st of -,-ast :-1-uropean :@ccessions, OEEAI.), LC, Vol. 5, No. 6 IT-re 1956, Uncl.

I SOV/1 24-57- 7 - 7596
Translation from: Referativnyy zhurnal. Niekhanika, 1957, Nr 7, p 18 (USSR)
AUTHOR: StanyUIV)Vidl, K. P.
TITLE: Some Laws Governing the Motion of a Gas Within Its Own Gravita-
tional Field ( Nekotoryye zakonomernosti dvizheniya gaza v sobst--
vennom pole tyazhesti)
PERIODICAL: V@ sb.: Mckhanika (MVTU, Vol 50). Moscow, Oboronciz, 1956,
pp 101-119
ABSTRACT: The first part ("The Motion of Highly Rarified Gases@') is dedicated
to the study of the motion of a particulate of gaseous medium in a high-
ly rarified state wherein the fundamental equations of gasdynamics may
be employed, taking into consideration the gravitational fields of the
particles and assuming that the pressure of the medium is zero, To-
tally disregarding the pressure, the author solves the one-dimensional
problem of the focusina of the particulate (or cold claseous) cloud under
the action of its own gravitational force. The one-dimensional motion
of a cylindrically symmetrical twisted mass of gas is studied. The
Card 1/3 pressures are disregarded and the gravitational force is taken as

I SON@/l 24-57- 7- 7596
Some Laws Governing the Motion of a Gas Within Its Own Gravitational Field
'speeds greater than the parabolical and may escape from the star. For a pre-
scribed density distribution of the scattering gas, the portion of mass that escapes
to infinity is determined. In the last part, the process of the propaDation of the
shock wave within the rotating gaseous mass is qualitatively discussed. The author
tentatively suggests that the process of the compression of a gaseous cloud and the
eruption of rotating gass masses under consideration could explain the formation
of the solar system. The work contains typographical errors.
M. L. Lidov
Card 3/3

Gas Dynamic Principles of Interior Ballistics (Cont.) 238
Calculation of the effect of the burn-out of de-
composition products 345
Period of gas expansion 348
Numerical examples 348
Method for the solution of the inverse problem 351
Particular cases 353
Numerical example 354
Supplement. Tables for Ch. VIII. 35T
AVAILABLE: Library of Congress BK/1sb
Card 10/10 27 May 1958
5 TA IV bi t@-O V
56-6-15/47
3tanyukovich, K. P-
@AUTHORS: Golitsyn, G. S. I
TITLE. Some Problems concerning Magneto-Gas-Dynathics in Consideration o@
Finite Conductivity (Nekotoryye voprosy magnitogazodinamiki s uche-
tom konechnoy provodimosti)
PERIODICAL: Zhurnal Eksperimentallnoy i Teoreticheskoy Fiziki, 1957, Vol. 33,
ITr 6, pp. 1417 - 1427 (USSR)
ABSTRACT. The above subject is dealt with by the following 5 chapterst
1: The equations used
2 @ The general properties of the systems of equations
3.@ Steady motion
4. Sliirht disturbances
5. Other methods for the investigation of slight disturbarces.
It is shown that the system of equations of magnet-gas-dynamics,
by taking account of finite conductivity, is a parabolic system.
If an approximated solution is introduced, which, of course, be-
longs already to the hyperbolic type, the characteristica herefore
are derived.
It is shown that the equation of a steady homogeneous current pro-
Card 1/2 cesses a certain critical point, at which the current velocity of

AUTHOR: STANYUKOVICH,K.P. PA 2232
TITLE: Some Unsteady Wo- and three-dimensional Gas Flows. (Nekotoryye
neustanovivshiye ploskiye i prostranstvennyye techenyya gaza#
Russian). -
PERIODICALt Doklady Akademii Nauk SSSR, 1957, Vol 112, Nr 4, pp 595 - 598,
(U.S.S.R )
Received; 4 / 1957 Reviewed: 4 / 1957
ABSTRACTs The present work investigates some types of isentropic gas flows
of the above-mentioned-kind. At first the system of equations
for plane gas flows is written down. Potential flows with
U .@WLX' v -WV are examined, and the following BERNOULLI
equation is obtainedi (@?/at) (q2/2) + i w 0, where
t f'lpq 2 1 ien Thus
"tions is oxamined

found in different prolz@.Tzaw -zut_e'1jw- af W*-As-
or the flow round some olanes. 2he ab*Te meaticz*1 iy3t--@vz of
equations is here specialined for tliis case. The 3333%-Yj *q7Lzt'!cxL
is several times transformed, on whic:hh occaslcz,
the independent and the dependent variables aze
In this wky a quasilirear equation of second order with rospect
Card 1/3

PA - 2232
Some Unsteady two- and three-dimensional Gas Flows.
another special case the generalized solution by PRANDTL-MAIER
for the flow round any profile or angle is obtained by a steady
gas flow. The here discussed solutions are suitable, among other
things, for the study of the flying apart of detonation products
in the case of detonations of figure charges.
ASSOCIATIONt Not given
PRESENTED BYs Member of the Academy BOGOLJUBOV,N.N.
SUBMITTED: 5-9-1956
AVAILABLE: Library of Congress
Card 3/3

GOLDOVPKIY, Yevse3r Mikbaylovicb, zagluzbenniy deyatel I nauki i tekhniki,
doktor tekhn.nauk, prof.-,8TAb*YWTIGH' Kirill Petrovich. doktor
tekhn.nauk, prof.; LTAFUNOV, Boris Val-e-r-fa-n-6VTch-,-i=h.;
DOSTUPOV, Boris Grigorlyevich, kand.tekbn.nauk; MAGAZANKIN, D.N.,
red.; LANINA, L.I., red.; BFJWV, A.P., tekhn.red.
(News of science and technology; from the materials of Sunday
lectures delivered at the Polytechnical Kuseum]@Xovoeti nai2ki i
tekhniki-, po materialam voskresnykh'chtenit Politekhaicbeskogo
muzeta. Moskva, Izd-vo "Znanie," 1958. 53 P@- (Vaesoiarnoe
obsbehestvo po rasprnstraneniiu politicheskikh t nEiuc1knVkh snanii.
Ser.4, nos.32/33) (MIR& 11:12)
OAntion pictures, Tbree-dimensional) (Calcalating machines)
(Interplanetary voyages)

5-rAN@VK0V)C,\-1 Y,-. 0-
10 (2); 28 (1) PHASE I BOOK EXPLOITATION sOV11603
Moscow. Vyssheye tekhnicheskoye uchilishche imeni Baumana
Nekotoryye voprosy mekhaniki; sbornik statey (Some Problems
in Mechanics; Collection of Articles) Moscow, Oborongiz,
1958. 197 p. (Series: Its [Trudy] vyp. 88) Number of
copies printed not given.
Ed. (Title page): V.I. Feodoslyev, Doctor of Technical Sciences,
Professor; Ed* (Inside book): A.S. Ginevskiy, Candidate of
Technical Sciences; Ed. of Publishing House: L. Ye Serebrennik;
Tech. Ed.: L.A. Garnukhina; Managing Ed.: A.S. Zaymovskaya,
Engineer.
PURPOSE: This collection is intended for scientific workers,
Aspirants and students of advanced courses who are interested
In problems of aero- and gas dynamics and in the theory of
directional control of aircraft.
COVERAGE: The collection contains reports on various problems
in lied mechanics. A large portion of the articles is
Card 178P
Some Problems in Mechanics (Cont.) SOV11603
devoted to aerodynamic and gas dynamic investigations. in
the first article of the collection, the author, Professor
K.P. StanYukovich, considers the laws of motion of a gas-drop-
let medium- in particular, the laws of motion of a mechanical
mixture of a liquid and a gas with liberation of energy. His
conclusions are applicable to the investigation of the motion
of a burning fluid jet. The two reports by N.F. Krasnov
deal with the aerodynamics of bodies of revolution. In the
first, he develops briefly the method of characteristics as
applied to the calculation of nonsymmetrical flow about bodies
of revolution. In his second report, which treats the base
drag of bodies of revolution moving at both subsonic and
supersonic speeds, he presents an approximate formula derived
for the calculation of the base-drag coefficient in the case
of turbulent flow about a body at supersonic speed. V, F.
Mikhaylina presents in her report the approximate formulas
she obtained for determining the distance between an isolated
compression shook and the vertex of a blunt-nosed body of
arbitrary form in supersonic flow, and also for determining
the velocity and pressure near the critical point. Professor
Panichkin presents in his report the partial and general so-
lutions of the differential equation used in the investigation
Card 2/8

Some Problems in Mechanics (Cont.) SOV11603
Mlm4avlev investigates the motion characteristics of one
of the automatic control systems used, especially in air-
craft and in ship's steering gears.
TABLE OF CONTENTS:
Preface
Stanyukovich, K.P., Doctor of Physical and Mathematical
Sere_n_c_es_,_7r_6Te_ssor. Some Problems of the Aerodynamics
of a Fluid Jet in Free Flight
1. Motion of a jet in a vacuum
2. Some remarks on the motion of a jet in a re-
sisting medium
3. Basic laws of motion of a gas in the presence
of intexmal energy sources
4. Basic laws of motion of a mechanical mixture
of a liquid and a gas
5. Basic laws of motion of a mechanical mixture
of a liquid and a gas with liberation of energy
Card 4/8
Some Problems in Mechanics (Cont.) say/1603
Krasnov, N.F., Candidate of Technical Sciences, Docent. On the
Method of Characteristics and Its Aplication to
the Calculation of the Pressure Distribution About Pointed
Bodies of Revolution Moving at Supersonic Speed at an
Angle of Attack 55
1. Accepted symbols 55
2. Characteristic equation 56
3. Conditions of conformity 60
4. Calculation of the flow about a body of
revolution at an angle of attack 67
Mikhaylina, V.F., Engineer. A Blunt-nosed Body of
Revolution With an Arbitrary Generatrix in Supersonic
Flow 76
1. Determination of the distance between the
compression shock and the body in a flow 76
2. Velocity and pressure distribution along the
aurface of the body of revolution near the
critical point 90
Card 5/8
3
5
5
12
21
35
47

Some Problems in Mechanics (Cont.) SOV/1603
yesiyev, M.K., Engineer. On the Problem of Determining
the Gas Dynamic Damping Moment 121
1. Description of the test setup 123
2. Sequence of the test procedure 135
Pobedonostsev, Yu. A., Doctor of Technical Sciencesp
and K. P. Stanyukovich, Doctor of Physical and Mathe-
matical Sciences, Professor. On the Calculation of the
Optimum Ratio of the Stages of a Multistage Rocket 144
Stanyukovich, K.P., Doctor of Physical and Mathematical
Sc1en__ce-s_,_T_r-o-fe-ss6r. Relativistic Generalization of
Tsiollkovskly's Formula 156
Shumilov, I.M., Candidate of Technical Sciences. Un-
sealed Pneumatic Control Mechanism With Cam Distri-
bution 162
1. Basic system of differential equations 162
2. Initial conditions 165
Card 7/8

29(l) PHASE I BOOK EXPLOITATION SOV/1235
Baum, Fillipp Abramovich, Kaplan, Samuil Aronovich, Stanyukovich,
Kirill Petrovich
Vvedeniye v kosmicheskuyu gazodinamiku (Introduction to Space Gas
IDynamics) Moscow, Fizmatgiz, 1958. 424 p. 4,000 copies printed.
Ed.: Fridman, V.Ya.; Tech. Ed.: Gavrilov, S.S.
PURPOSE: The purpose of this book is to present to astronomers and
physicists the most advanced methods of gas dynamics, to be used
for solving various astrophyzical and physical problems.
COVERAGE: The book is divided into three parts, each of which is
essentially complete within itself. The first part presents the
fundamentals of gas dynamics as applied to the motions of cosmic.
gaseous masses in the absence of magnetic fields. Included In this
part are the theory of shock waves and the theory of unsteady
motions of a gas, the main emphasis being on the motions of a gas
in a gravitational field. The applications of theoretidal methods
to nonstationary stars and to various geophysical problems are given.
Card 1/ 9

Introduction to Space (Cont.) SOV/1235
TABLE OF CONTENTS:
Preface 7
PART I.,, SPACE GAS DYNAMICS 11
Ch. I. Equations of Space Gas Dynamics 11
1- Equations of motion in space gas dynamics 11
Ch. II. S4bck Waves 15
2. Elementary theory of shock waves i5
3. Two-dimensional straight shock waves and their properties 22
4. Structure of shock waves 31
5. Straight reflection of shock waves 34
Ch. III. Oblique Shock Waves 36
6. Derivation of the basic relationships 36
7. Reflection of oblique shock waves 45
Ch. IV. Collisions Of Gaseous Masses And Solid Bodies 57
Card 3/9

Introduction to Space (Cont.) SOV/1235
16. Reflection of a rarefaction wave. Two-sided dispersion' 102
17. Redistribution of the energy and impulse'in a non-
stationary flow
18. Dispereion of a gas in the case of resistance of the
external, medium
19. Three-dimensional motions. Problem of a strong explosion 117
Ch. VII. Motion Of A Gas In A Gravitational Field 130
20. Steady-state motions of a gas in the gravitational field 130
.21. Dynamically similar motions in a characteristic
gravitational field 137
22. Unsteady one-dimensional motions in a gravitational field
1 , 141
Ch. VIII. Some Problems In The Gas Dynamics Of Nonstationary
Stars 150
23. Several methods for solving the problems of the Inotion
of gas in stars 150
24. Various cases of motion of the gas in stars 157
C.,ard 5/ 9
Introduction to Space (Cont.) SOV/1235
Ch. IX. -Geophysical Supplements To Gas Dynamics Methods 176
25. Motion of meteoritic bodies in the atmosphere 176
26'. Impact of meteorites on the surface of a planet i9l
27. on the nature of the earth's volcanism 201
References 20a
PART II. MAGNETOGASDYNAMICS
Introduction 209
Ch. t. Equations Of Magnetogasdynamics 212
1. Equations of motion. Change in the intensity of a
magnetic field during motion of the gas 212
2. Solution of the equations of magnetogasdynamics in the
case of unsteady one-dimensional motion 219
3. Motion of a gas in an electromagnetic field. Char-
acteris, Ucs of the'equations for a medium with finite
conductivity 222
3a@ Dynamically similar motions in a medium with finite
conductivity 235
Card 6/ 9

Introduction to Space (Cont.) SOV/1235
12. In@roductory remarks 278
13. Correlational equations of the statistical theory of
isotropic hydromagnetic turbulence 287
14. On the solution of the c orrelational equations 291
15. Lbytsyariskiyls invariant j297
16. Relationship between the pressures, temperatures, and
other parameters in the case of isotropic hydromagnetic
turbulence 300
Ch. V. Statistical Theory Of Isotropic Gas Magnetip Turbulence.
Spectral Method 305
17- Spectral functions 305
18. Spectral equations 308
19. Solution of the spectral equations of isotropic gaB
magnetic turbulence for the stationary case 315
20. Solution of the spectral equations of nonstationary
isotropic gas magnetic turbulence 32'2
21. Spectral functions of isotropic gasmagnetic turbulence 331
22. 'Chandrase kar's theory for hydromagnetic turbulence 337
23r Turbulenc e under interstellar conditions 340
References 346
Card 8/ 9
or a conaucTing-m6cuum-- ---387
6. Elements of the shock-wave theory 396
Ch. III. Problems Of Motion Of A Medium In The Relativistic
Casp 1 1 410
7. Dispersion of a gas 410
8. Sound waves 421
References 424
AVAILABLE: Library of Congress
- IS/nah
Card 9/9 2-25-59

SO"494
PUS3 I BOOK EXPLOrrATION
Vasil 0yov, )Ukhail Vasiltyevioh, and Sargey ZakhiLrovich OashchOv
Reportazh iz XXI voka; my zapisall rasokeZy dviulteati devyati
scvetakikh uchanykh a naake I takhnike baduahcheec (Reports
From the Twenty-First Century; Storie3 or r."Onty-111ne Soviet
Scientists an Science and Engineering or the FXturo) (140000WI
lzd-vo Sovat5kaya Roamiya, 19 50,000 copies printed.
58. 243 P.
Ed.: V. A. Oolubkova; Tech. Ed.: '0, 1. laayav&.
?URPOS3 z This book In Intended for the gentral reader,
COVERMS; The book contains 27 articles (told reporters by
Soviet scidntlat3) dealing with probable rutura proZro33 In
physics, chemistry, electricity, r@atallurgy, en,7inadrinc-,
mining, medicine, biolcZy, a4,ricultu", zoolo@,,y I transportation,
exploration Of space, and phatorraphy. Attention 13 given to
automation, .1to:43tie underground gasification Of coal, use of
now matala,modarnization of oil fields, stoulc electric stations,
production or motal parts by the process of explosion, explo*ions
card-III
Reports From the Twenty-First (Cont.) SOV/5494
in dam Construction, cancer, internal longevity reserves,
machine dISZnaaes of illnezace, surZery vs. treatm3nt by, ultra-
Sonic vibrations, =OchwLical heart au@)3tltutog, bu:--')n body b,-%!@,
'010diOaa OngiAtOrIna.11' enriched fod,11r, lsuporfartilizor3*,
ficial. Anouralle, agriculturc Va. -M-l,ultr,.. radjoah@7-ist-
y,
POWOP b6La VS. wire, machines dolnS Into.11octuAl work, :Lil auto_
Mobil*4" (with 'radio zotc,W), 'artifiGI3.1 Sun* (Oleotromag-
OOtIO r , focused above a citr which 0a"o basted molecules
to n eT
Shl , future OCOan Ships rallWay dre2dnoaZhts1, 1,ioscow
of the ratux1a, movins pavomtni., Wh*Ollesm And driverless auto-
mobiles, electric cc,,c,3r&3, the Inductrialtzgtion of Sibaria,.
use Of underground beat, Climate controlglivina on the moon,
antimatter, and photon jet. 11=01 If the interviewed oc@antist3
are given. There are no references.
TABLE OF COInTh'TS,
IMMODUCTION
Plopion Into the Future
5
ROPOrts Prom the Twentyy1rat (Cont.) 3OV/5494
Learn to D&-am (A. W- NGMOYanov, Academician) 10
THE YUXDAM=AL'AND MOST XMpCaTpXT ?M,33
Transforsation Of 2
Bard1n, Ac&damiaj&nlS`0O t9 -- t2le Pature of Metalurg,
n 'y M P.
V160-Prooldont, As iussRl
25
FAnaf Are BrOlthIng Their Last [I. S. Q&rkasha, Director of
vffiOOOyu=YY nauchno-lool dovatel-skly Inatitut opod,cameax"
I I
Al -Union Scientific ROO arch natituto of Undergro=a Gasirl.
eatiOn Or CORI -- and 31. A. 7adaroys DftPut7 DIrOator *rQr, the
841411tIfic Section)
34
WAUtaftatic Oil Pield IS. 1. Mironov, Aca4emlaLaa, and K4 Al
.amber, AS VSSRj 45
ft*m the SwAr"s (A- VIUt4r Academician 1 51
Caft 3/7
C7

XD
"OV/139-58-6-3/29
AUTHORS: Orlenko, L.P. and 'Stanyukovich, K,,P.
TIIPM : Shock Waves in Solids (Udarnyye volny v tverdykh telakh)
PEttIODICAL:Izvestiya Vysshikh Uchebnykh Zavedeniy, Fizikaa,
19581 Nr 6$ pp 14-24 (USSR)
ABO'J'TRACT: A theory is presented of the propagation of shock
waves in solids; a relation between instantaneous
pressure and deformation is deduced and -the
corresponding wave and particle velocities computed,,
The basic equation of propagation in one dimension is
au + -@k 0, ou, av (1)
@_t ah Zh Z@t
Here u aenotes the particle velocity, v = specific
volume (v = 1/p, where p = density) and h the lia-g-rangian
-0-oidinate; t and p denote time and pressure
respectively. Writing a for tension and s for volume
strain (i.e. change in volume per unit initial volume)
the following relations are obtained:
a = -b, v - 70 = 'R 0 1. (2)
Card 1/4 vo P

SOV/'---'39--8-6,.-z 420
Shock Waves in Solias 11 -@/ 4@2
Here vo si&uifies the initial value of v, while P and
Po sill, fy the densities associated with v and vo by
v = 1/j-@ and vo=1/@'o respectively. Substitution of
Eq (2) into Eq (1) yields the fo'Llowing relations
4u, D a d, a ;5 F, 3 U @'e
at - Z#h VO -5-F,
If the relation between a and. e is Imown in functional
form, these last equations enable the shock-wa:ve
velocity te be deduced. A relation which gi-ves good
agreement with experiment is:
a - 00 = -A(s - eo)--3
(4)
where 1901 6. are initial values of a9 E; and A is
related to the elastic propertuies of the medium. The
shock-wave velocity c, associated with this relationship
bet'Ween a and- e I is readily shown to be given by:
+ (6)
rep + e.0 2
Card 2/4 1 P

Shock Waves in Solids SOV/139-58-6-3/29
and the corresponding particle velocity w is gi-ven by:
W 7@A 1 2. (?)
J00 (1 + 60
The theory is used to discuss the case in which the
initial disturbance lies outside the medium, the example
chosen be g that of an explosive charge detonated at
a height. t above a plane boundary of the medium. The
pressure, p, at any time t after the explosion in this
case follows a power law given by
P - Po 3n (29)
PH - Po
Here pTT is the value of p at h = 0 and t = 0 respectively;
an7e
n are empirical constants and T is a
po
characteristic time t/1), where D is the detonation
velocity [no numerioal results are given j-n co,, etion
Card 3/4 with this example but it would presumably be applicable

Shock 1,11aves in Solids
SOV/139-58-6-3/29
to a "nuclear device" detonated above the earrIals
su-rfacej. The theory is then applied, to a plate of
thickness d and waves reflected from the rear surface
of the plate are discussed, There. is 1 figu-re and
1 Soviet reference..
A'-O'SOCIA.TlOl,l:l,~toskovskoye Vyssheye Tekbniclaeskoye Uchi.1-'shche
imeni Baumana (Moscow Higher Technical imeni
Bauman)
SUB14ITTIED: 16th April 1958
Card 4/4

VASILIYEV, i-M.;GUSHCHEV, S.,-NNSMLTANOV, A.N.. almdemik; SHCHKRBAKOV, D.L.akademik;
ENGELIGARDT, V.A., akiidemik; ZHEREBAK. A.R.. prof.; UB=V. S.A..
akader--'@--; ZINKEVICH, L.A.;.GRAIDOV, A.S.; GOLODOVSKITi N.G.. prof.;
STO",
i ;!Sv I @ pro f
Ahead with the dream! Znah.sila 33 no.12:24-25 D '58.
(MIRA li.-12)
1. Chlen-korrespondept AN SSSR (for Zendevich). 2. Direktor Ysuchws.
Issledovatellskogo Instituta proyektirovantya obishchestvenafth Zdanly
i sooruzheniy (for Gradov).
(science)