SCIENTIFIC ABSTRACT SHVEYKIN, V.V. - SHVEYTSER, YE.K.

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• Collection: Scientific Abstracts
• Document Number (FOIA) /ESDN (CREST): CIA-RDP86-00513R001550410019-5
• Release Decision: RIF
• Original Classification: S
• Document Page Count: 100
• Document Creation Date: November 2, 2016
• Document Release Date: March 14, 2001
• Sequence Number: 19
• Publication Date: December 31, 1967
• Content Type: SCIENTIFIC ABSTRACT

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SMYKIN. V.V. prof. k1oktor tel-hn. nauk- GUN, G.Ya., inzh.
Changes in tube wall thickness duri ng the process of rotary swaging
without mandrels. Izv. vys. ucheb. zav.; chern. met. 2 no.4:57-64
Ap 159. (MIRA 12:8)
1.Ural'skiy politekhnicheakiy inatitut. Rakomendovanokafedroy
obrabotki metallov davlenlyem Urallskogo politakhnicheakogo instituta.
(Tubes) (Forging)
Awl

ORLOV, S.I...inzh.-, Ooktor fek~jn.W-111-
C)iaracteristics of plastic dofnrmation in transverse upsetting,
transverse and spiral rolling. Izv.vvs.uch,-b.zav.; chern.,iet. 21
no.~:55-68 It 159. 4i-JRA 12:9)
1. Ural'skiy politRkbnicbeskly institilt-,4.,
(Defor~ntions (Mechanics)) (Rclling (14ntahroi~k,))

SMYKIII, Y.Y. -. STMCH. A.G. -, BTKOV, V.D.
Production of thick-walled titanium pipe blanks. Izv.vys.ucheb.
zav.; tavot.met. 2 no.6:178-184 '59- (MIRA 13:4)
1. Ural'skly politakhnicbeakiy institut, kafedra obrabotki
metallov davlanirom.
(Titanium) (Deep drawing (Metalwork))

SHTEYKIN, V.V., doktor takhn.Dauk; GUN, G.Ya., inzh.
Analytical method of determining unit pressure in pipe rolling
without mandrels. Obr. met. davl. no.5:175-178 159.
(MIRA 13:3)
1.Ural'skiy politakhnicheski7 institut.
(Rolling (Metalwork))

SOV- /214 -~3 -6 0 - I
AUTFORS: Orlov, S. 1. , V.
TITLE: Deformation of Cylindrical. Bodies Di-iring Repeated
Transverse Upsetting

PERIODTCAL; I
Izvestiya %ysshikh uchebny'kh zavedeniy. Chernaya
m,--taliurElda, 1960, Nr 1, PP 108-115 (USSR)
ABSTRACT: Tnis study of the distrjJ~,~&ion of deformation during
repeated upsetting waz wadocted on the samples T,-jhich
-.,,,ere soldered from the parts ha-ving a coordinate network.
The quadratic net,.-;ork 3x3 mm vias applied to the surfaces
of J-ead samples ;jith an accuracy of 0.1 mm. The repeated
uosettin,-- 'v;as performed between the smooth, flat parallel
dies of a hlydraulic press. After the deformation and
m,eas:Ur*nF,, -,-h-e sar,,iples viere heated up to about 1000 C1
,unsoldered, cleaned, and measured again. The length and
~.-he angle of distortion of the deformed net- .'iork were
mea3*ured i'-'y mi.croscope ':~o an acc'uracy of 0.01 mm' and
Card 1/- 10, In tne study of distribution of delormation during

C d r i c a I Bo d i e 3 D; ri 1 7 70' 9 5
reduclions 6 Llhe sample rned -4!
same r_irec'_-.-o,-,Ior, 3-6 ancrie be-fore every consecu-
'--3.,e reducticn. The character of deformation in cross
z;ecEicns is shown in Pig. 2. Sample 61 was subject to
indi',,Iclual reductions. The deformation in longi-
,:.zdinal cross section is shown in Pig. 4. The distri-
b~_'Itlion of' plastic deformation during upsetting with a
-~I,rn of -90' is ill,,.istrated in Pia-. 5. The stressed
_.,-,,'di~ion of axial la,rers of metal is illustrated in
Fi~!, As a result of experiments conducted the author.-
sta-e that in the axial zone of the billet there exists
a %,~ol,-u-net--ic state of stress (of opposite signs) con-
31_-~- ing of compreplM stresses along the line of action
r-X 2.-~ternal loads and tensile stresses in two other
directions, and that the tensile stresses, acting in
~-he crcss section perpendicularly to the compression
C)i-ces, are the largest. During the rotation of the
billet around t'ne axis, the idnae vol'ume of the axial
parr- of the billet passes r-twoeugh the constant field
cr' stresses and is subject to alternate action of

of t-he angle of distortior, of See-
L Lrlo.', oil cl is-lcs 1, 5, and C) of
i-,l ana in dia!,.ietr-r by 0.52;b and
--o of tho ~;amrjle (disk 1);
mli! C, (-j,ll f"ace 5); x x = 76 mra f rom face
d

-S 5 t 7 i5o t ~y 6117
1 q a c J- oris
~S Ff 2V 27 10 33 35 3:7 JZ .25 iJ 57 W 53 M -Z Z,,

V~
0,03-
10,02 -
00/ -
0-
100/
-10
34 1--tile t imi
6 9 42 1(5 .13 2Y 24, Z,..v,-r
Fi(-". 5. ol' deformation of cells of long..--
tt'(1Lnal -c,~)rdLnate ntAv.,rrl.-l in tht~ direction z-z durin.-
t.h~; tt.-;c, miii-t-tally p'z.rpendicular rl~ducbiono to 2.1; 5.5
a.ld first reduction; x second
It redue 'L io n.
5 IT

L o r,, C:I-,i 1! 1 d r La 1 Do (A -L D,
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6. A dial-,ram o[' axial Cibers by

aeformation ol" Cyl;'-ndrical Bodies D'-irin- -i7695
n . 0
ReDeated TranS7erse Upsetting SOV/'!48-6o-,L-i8/34
ASSOCIATION~-
SUBMITTED:
compressive and tensile stresses. Consequently, when
a definite value of the transverse deformation and
stresses (for a given-:,"Amr-i2,14 * is reached, the
continuity in the axial zone is disrupted. The previous
work cX Unksov, Frokht, and V. S. Smirnof is mentioned.
Tfierc~ are 7 1'igL1r'eS; arid 4 Sovlet t,eferences.
Ural Poly technic Institute (Urallskiy politelchnicheskiy
institut)
October 25, 1958
Ca, rd

M
--4F
SHUYKIN, 'I. V.
lfficient shape of piercing mill mandrelae Izv. vys. ucheb. sav.;
cherne met* noo8:81-87 060. (KIRA 13: 9)
1. Urallskly politekhnicheakiy inatitut.
(Rolling mills-Squipment and aupplide)

S/148/61/000/002/',X-15~/
A16l/A133
AUTHORS: Shvnykin, V.V., Ivshin, F. N., Karpenko, L. N.
Tr=: Experimental determination of pressures and axial slip coefficient in
the piercing of large ingots
MIODICAL: Izvestiya vysshikh uchebnykh zavedeniy. Chemaya metallurgiya, no. 2,
ig6i, 62 - 67
TXXT:~ The results are given of an experimental investigation of the axial
91 slip in the shell in the piercing mill process with mandrels of different gage,
carried out at the Chelyabinzkly truboprokatnyy zavod (Chelyabinsk Tube Rolling
40t Plant). The purpose was -o find cut the metal pressure on the sill rolls andthe
the mandrel in rolling with new standard roll gages ( Yno (Uk)) that'han replaced
(hr's since 1959 the old "UPI" of,1954. Ingots with 547/531 and 615/500 mm diameters
0822J (i.e, diameters of the botto'm and top ingot ends) were pierced on 375 and 425 mm
,Veel diameter mandrels of "20" and CF-A (St-D) steel. TLie slip was studied simultane_
kbe'S ously as to its conside*rable effect on the metal pressure and its dependence on
the pressure. It was determined by marks made on the mandrel rod and on the water
C42W feed pipe above it, and measuring the mean time during which the shell passed every
V
Card 1/3
'V02---
efe.~'e~c 2ed
e,s. IF

S/148/61/000/002/005/01!
Experimental determination of pressures and ... A161/A133
ASSOCIATION: Uraltskiy pollteknnicheskiy ingtitut (Ural Polytechriioal Institute)
and Chelyabinskly trubnyy ;avod (Chelyabinsk Tube Plant)
SUMITTV: January 29, 1960
Card -3/3

SHVp~yKIN, v,V. Drof , , do.Ctor t.F?klrir . nauk; SKORNYAKOV, V, K , a ~L3115" er,-.,
ka.=-', t-ez(hn. nauk
PrInc4-"es of -~he modern theory of defcrmatior, and streSses -*n
r, -
zr.z7es rul-Ling and screw rolling. Sbr-r. nauch,. trud~ Ural,.
polifekh, Anst. no.122&243-25) 16!~ ( MY RA 1,77 i 12 ;~

3/133/61/000/003/010/014
A054/AO33
AUTHORS: Shveykin, V. V., Professor, Doctor of Technical Scienf'.eq;
-or l. 0.v I Engineer; Karpenko, L. N., Engineer
TITLE: Improving the roll-pass designs and mandrels for piercing
large ingots
PERIODICAL: Stall, no. 3, 1961, 256 - 259
TEXT: To investigate the principal factors affecting the operation of
the piercing mill tests were carried out with the cooperation of P. N. IJ
Ivshin, Engineer, to improve the roll-pass designs and mandrels with the
purpose: 1) to obtain the smallest possible reduction before the mandrel
front piece; 2) to increase the length of deformation focus in the p-'erc-
ing cone; 3) to use piercing mandrels with a shaping nose having an a7erage
angle of inclination of 10 - 120; 4) to apply small angles of inclination
of the shaping cone of lateral rolling. As it is not easy to increase
roll barrel, the new roll-pass design of the piercing cone has two stages.
In the first stage the shaping piercing cane has a great angle of inclina-
-A 1/6

S/133/61/000/003/010/014
Improving the roll-pass designs A054/AO33
tion (40). This is necessary to equalize the diameter of the multi-edged V
billet crosswise and lengthwise. In the second stage the angle of incli-
nation of the effective area of the piercing cone is 2030T as compared to
3015' in the conventional roll-pass design. The maximum roll diameter is
64 mm. nearer to the piercing cone to make it possible to use elongated man-
drels. The angles of inclination of the shaping cone are calculated in
such a way that the diametrical reduction of the billet before the mandrel
nose is at least 5 %, provided this end coincides with the area of contrac-
tion. The angle of the shaping cone in transversal rolling was taken as 20;
in this way the diameter of the pierced tube blank is approximately equal
to the average diameter of the billet. The profile of the mandrel was
designed for three positions: 1) when its nose coincides with the contrac-
tion area; 2) when it is 30 mm and 3) when it is 60 mm. ahead of the con-
traction area. When the nose of the mandrel coincides with the contraction
area, the coefficient of relative reduction of the wall can be calculated
by means of the following formula:
S
S 'qred (4)
Card 2/6 t.b.

S/J33/61/000/003/010/014
Improving the roll-pa3s designs A054/AO33
where So = initial wall-thickness in the plane of the front piece of the
mandrel, St b = wall-thickness of the finished tube blank, rbred - coef,
ficient of ;eiative reduction of the wall. FAbstractor.s note: subscripts
t.b., red. (tube blank, reduction) are translations of the original r,
_F9T_1'z_aT_and Od (obzhatiye)j. The diameter of the tube blank in each sec-
tion can be calculated from
D D + 2 x tgat (8)
i 0 COSP
where x = distance from the origin of the coordinate, ck angle of taper of
the rolls in the cone of piercing or transverse rolling, --, angle of in-
clination of the rolls towards the direction of rolling. The diameter of
the mandrel in each section can be drived from
d D. - 2s.
(9)
where s = wall-thickness. The new YRO-59 (UPI-59) roll-pass design has
been tested mainly on 1511 diameter billets, pierced with three kinds of
Card 3/6

3/133/61/000/003/010/014
Improving the roll-pass designs .... A054/AO33
mandrels a) short (1 = 536 mm; average angle of inclination of the shaping
nose of the mandrel: 220); b) mediumsized (I = 566 mm band 200) and c)
long mandrels (1 = 598 mm and 180). During the tests the following values
were determined: billet dimension, its temperature when discharged from
the furnace, heating time, duration of transport to the stand and of pierc-
ing, the length of the tube blank, piercing temperature, the rate at which
the tube blanks are discharged from the standithe metal pressure on the
working rolls and the mandrel, voltage in the winding of motor-rotor. Table
I shows that optimum results were obtained with the medium-length mandrel,
(568 mm: lower specific power consumption, (12 %), increase in the piercing
speed, i.e., in the output of the piercing M-111) by 10 - 12 % and inbreases
in the output of faultless (1st class) tubes: 93 -- 95 % instead of 87 - 90%
obtained with the old-roll-pass design. There are 4 figures, 1 table and
1 Soviet reference.
ASSOCIATION: Ural'skiy politekhnicheskiy institut (The Ural Polytechnical
Institute) and Chelyabinskiy trubnyy zavod (Chelyabinsk Tube
Plant)
Card 4/6

ImprovinIrl, the roll-pass designs ....
Table 1
,I Comparison of the operational
7
parameters of piercing mill. man-
drels according to the UPI-59 and
UPI-54 roll-pass designs; 0 Roll-
-pass design; Length of man-
drel, mm; Steel grade;
(~) Ve-
locity of piercing mm/sec; t. Pow-
er consumption kwh/t, (7) Piercing
15"-diameter billets; (q) Piercing
17"-dia:aeter billets; (9, + In
brackets: acceleration in the ne%v
roll-pass design as compared with
the old, in ci"; (00 ++ In brackets:
decrease in power consumption, ac-
cordin.m to the new roll-pass design,
" ; --,
n
/W - UPI-54; V UPI-59;
UPI-54; (&. UPI-59
Card 6/6
S/133/61/000/003/OlO/Oi4
A054/AO33
COMMBAeHve ROKaSaTeiieh padoni NHCTPYMFHTa
npOLUROmoro CTa"a no KaAH6PO5Kam Ynit-59 ti Y[Itt-54
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0 r]H_59 568 20 36.6(+ 18 4) 13 2(-12.2)
y 593 20 36.6 (+18:4) 13:9 (-11,9)
538 a 34,9 (+19,9) 14,4 (-11.1)
568 14,15 (-12,4)
AD OLLIPOWHM CARTK8 Allam. 17 Aiofl.%ion
Yn14-54 I - 1 J20 28 7
24:3
ynkl-59 538
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B cx xax-ycPcopeHHe upw HoooR xmirRiSpoexe no cpasseuRm co
crapoft. %.
(Do *1 B CKOOKOX-CHUMeRHe PaCXOAS mprmn npm nepezoAt nfi Ho-
BY10 Kail"45poaKy. % 7-c?A /,

SHVEYKIN, V.V.; BISK, M.B.
Geometry of floating mandrels for tube drawing. Trudy Ural.
politekh. inst. no.127:56-64 161. (MIRA 16:8)
1. Ural'skiy politekhmicheskiy institut (for Shveykin).
2. Sinarskiy trubnyy zavod (for Bisk).

SVEIKIN, V.V. [Shveykin, V.V.]; SKORNEAKOV, V.B. [Skornyakov, V.B.]
Use of the optical polarization method In the study of the
deformations and tensions in transversal lamination. Analele
w metalurgie 16 no.4:122-129 O-D 162.

SHVMIN, V. V.,- IVSHIN, P. N.
Changes in Pipe wall thickness during its rolling vithout,
mandrel. Izv. vys. ucheb. zav.; chern. met. 5 no.12:67-73
162. (MMA 16: 1)
1. Ural'skiy politekhnicheBkiy institut.
(Rolji~(Metalwork))

BISK, Natve Viktor Vasillyevich; ORLOV, S.I., kand.
,y Borisovich; LHVEYKIN,
tekhn.nauk, retsenzeni--, _TSYMEML_1STV_N.N.-,- red.; MALIKOVA, N.T.,
tekhn. red.
(Pipe draying on self-centering mandrels] Volochenie trub n&
samoustanavlivaiushebeisia opravke. Moskva, Metallurgisdat,
1963. 126 p. (MIRA 16t6)
(Drawing (Metalwork))

SMTEYKIN, V.V.; SLAVD-1, V.B.
InvestiF!atin~: stre SSeS 4 n -he fc,-c4n:~ 2r a tj'D'-- -h-cu--gh the
tjols of a die. izv. lrys. ucheb. za*,r.; chern. rne7~. 6 no.F:
721-81 163. (MIRA 16):11)
1. UrqlIskiy !-!o-liteklinicheskiy in-';!J'I*,it a Si-ntjrsk-;,y tl-ubny'f
zavod.

SHVEYKIN, V.V.; BISK, M.B.
Determination of the maximum reduction in pipe drawing. Izv. vys.
ucheb. zav.; chern. met. 6 no.10:88-94 163. ()CERA 16:12)
1. Urallskiy politekhnicheskiy institut i Sinarskiy trubnyy zavod.

SHVEYKINY V.V.; BISK, M.B.
Elements in the theor-j of tube drawing in colls. Izv. vys.
ucheb. zav.; chern~ me'~. 6 no.12:99-108 763.
(MM 17 - 1)
1. Urallskiy politekhnicheskiy institut i Sinarskiy trubnyy
zavod.

BISK, M.B.; SOMINSKIY, Z.A.- SHVEYKIN, V.V.
P
Tube drawing with self-centering mandrels on rectilinear-type mills.
Stall 23 no.6036-540 A 163. (MA 16:10)
1. Sinarskiy trubnyy zavod i Urallskiy politekhnicheskiy institut.

SHVEYKIN, V.V.; IVSHIPI, P,N.
Deformation of tubes without mandrels. Izv. vys. ucheb. zav.;
chern. met. 7 no.1:123-130 164. (MIRA 17:2)
1. Urallskiy politekhnicheskiy institut.

SHVEYKINY V.V.; SLAVIN, V.B.
Deformation during the pushing of a pipe through a the hole.
Izv. vys. ucheb. zav.; chern. met. 7 no.2:86-93 164.
(MIRA 17:3)
1. Urallskiy politekhnicheskiy institut.

1~
OH116"Y"I'l IN , V. V . ; Gi~ It' , "' . Ya. ; iV,;f 1111 , P. N.
.abiliLy of rhe sect.~onal. shape of' a plpe during redlicLion.
Izv,v- 4:88-92
ys.ucheb.zav.; chern-i;:et, ? no. t0"4. OMIRA 17: 5)
1. l,ral'.-;k-iy politeklin-ic-heskiy institut.

1;
cilang s in the ~:~-ness of -Z; wa - 's
or, lhe. tougimess and pllastic.4ty harden ric-
vys. ut,~heb. zav.; cner::. met. 7
-y poht.akhnicheskiy `nstlt.ut.

, I I V 1'. ~ t, I i, I,J . I . . I V "' H 1 N p v . N .
, , i I .
deforzatior, duri:w 3-3duct-,oll wlthout, tt "irld e1
Izv. vvs. ucheb. zav.; rhern. rre~. 7 '64.
(m:""A 1,?:q)
" I
- Urillok-41,- t;o1il.e0michesk-Y nzt-Wt.

,Iivi,~Yvirl, V.V.; 1UHH-1,
,g or. the degree (if' ova'it,y r-jf the g-r,)Gves
Pipe elongation depend 4 F
and the number of rolls in the reduction mill stand. izv. vys.
ucheb. zav.; chern. met. 7 no.10:92-97 164.
(MIPA .17: 11)
1. Urallskiy politekhnicheskiy institut.

Sil-VEYK124, V.V.; ORLOV, S.I.; KAUP-MM, 1-1.11.; STOLSTINIY, N.F.; NODKV, E.O.
STMi9 V. A.; OFJDV, V.A.
Guillotine ahears for the hot cutting of rclmd ingots. Metallurg
9 no.1-.35-36 Ja t64 NIPA 18:1)
1. Ural'skiy politekhnicheskiy institut, Urallskiy nauchno-issle-
dovatellskiy i-rstitut chernykh metallov i Petrourallskiy novo-
tmInyy zavod.

BISK, M.B.; SHVEYKIII, 7 . TI .
bopur.d,mce, (if t1hc. shape and position r," c?ie
in the area of defor:nation on Lhe par,,mebvi t;f I,w, (IrriwIfIjf7
process. Stall 24 no.11:102'2-1024 N7 164.
1. '~inarskiy trubnyy zavod i pol"tekhrii-I., - : c 4 ., ~ !I ~
-, ~: I - _ ; _,:.:,i ZU t .

~f- -1hapol tubea.
OMIRA 1818)
p

S HVLYKVA, R. V.
USSR/Biology Biochemistry
Card
Authors Yurkevich, V. V... and Shveykina, R. V.
Title Formation of active invertin in Saccharomyces Globosus
Periodical Dokl. AN SSSR, 97, Ed. 21 297 - 300, July 1954
Abstract Experirmntal data show that the largest formation of invertin is observed
during the action of fructose. This confirms the assumption that fruc-
tose and not saccharose has a specific effect on the formation of inver-
tin. This also gives proof of the affinity of yeast invertin toward
fructose. Ten references. Tables.
Institution The A. M. Gorkiy Ural State University, Sverdlovsk
Presented by Academician A. I. Oparin, May 14, 1954

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(I t _i --) , , ,
.-l te -.r- ca---i-ied out wi '"i tit nil u:- hylrn-~ide
1 ) TI-,;- ex t ac i o n 'A.-, --v e e o '- coll;D4- 11 s e x -
t t- r~ r 1 2 t _i o n o c a! i e y s u, f -, i c e -a c t -;' v e
ces; 2) it founrl, t',~at in the pr.-sence
of -i.,o---:Yl :t!'d n-butyl ~~lcohol the extraction
r, 2,-- v:- y c-., r d C
;r colloid-A ;)-rti 'es is
incre.-.se~ , v.",er-r-as t',Ie extraction de,---ree of pocitively
c."ilr --ed ,-irti c! e~,; i!~ lecreased 3) Alcohols aOled to
t'ne (without del-.tin~ for- an unst~;bl,:~
t,~ not -"Je- to exti-ot t~ie t1io-"C.-rse ph:-.se
:-olutions. T~1(jrc :,~---e J fip%res, I table, and
7 rl-fe.re..ce.--, 2 of which are Soviet.

-5
'!"-f ---e-Ac tive Su,- - t a, ce.,j U_,-~nr: sov I: - 5s /2' 2
I - d I r t --' c 1 c t t h c- I - ' e s e. S rfa- e : L 4 ~2
10 71 Ur,--1'5'!--iy politc-L-,hnicheskiy instuitut i M. S. IL K~. - c va
(U:t----'L -'olytocnrical I.,lst .4tute i.-eni S.--`.Kir~jv) K-,fe,ir-n
Z; ('~ I-- J, "
of Ph--~;ic-l
0
T.,
Oct~-,-er 14, V157

AUTHORS: Sh,veykina, R.V.; Mokrushin, S.G. 69-58-2 -18/23
TITLE: The Effect of Electrolytes on the Coagulation of Colloid
Particles at the Liquid-Gas Interface (Vliyaniye elekro-
litov na koagulyatsiyu kolloidnykh chastits na rezhfaznoy
pove-rkhnoeti zhidkostl-gaz)
PERIODICALs Kolloidnyy zhurnal, 1958, Vol XX, Nr 2, pp 233-256 (USSR)
ABSTRACT: Colloid particles of silver, gold, arsenic, antimony sols,
etc., have been extracted from solutions by means of gela-
tine foam ~_Ref 1_7. This method is also useful in separat-
ing colloidally and molecularly dissolved substances. The
colloidal particles a2quire a surface active character after
the addition of gelatine. They move spontaneously to the
interface liquid-gas. The process is considerably influenc-
ed by the presence of electrolytes. The electrolytes in-
crease the foam formation ~_Ref 4-6~. The electrolytes
studied were KN03, NaNO3, LiN03P Ba N03)2, AI(NO3)3' Zr
~N03)4 , etc. Figure 1 shows that the degree of extraction
increases with the presence of an electrolyte.Bivalent ca-
tions cause a greatei increase than monovalent cations.
Card 112 Ions with three and four valencies cause a reduction. The

69-58-2 -18/2A
The Effect of Electrolytes on tne Coagulation of Colloid Particles at the
Liquid-Gas Interface
most effective among the monovalent ions Li+, Na+, and K +
were the Li ions, because they had th(,
hi6he3t deeree of hydration. The degree of extraction is
connected with the aggregation of the colloid particles
under the influence of electrolytes and with the foam pro-
ducin6 capacity of gelatine.
There are 5 graphs and 7 Soviet references.
ASSOCIATION: Ural'3kiy politekhnicheskiy institut imeni S.M. Kirovap
Sverdlovsk (Ural Polytechnical Institute imeni S.Y. Kirov
Sverdlovsk)
SUBMITTED: January 5, 1957
1. Colloids--Separation--Me'uhods 2. Gelatine-Foam--Applications
3. Electrolytes--Applications
Card 212

SHVEYKINA, R. V. : Mlastar Chern Sci (diss) -- "'che Idnetics of foam iaxtractLon
of the clispcrsion phase of hydrosols". Sverdlovsk, ~959. 16 vp (11.1in Higher
0
--Wac 'TSSTt, lira! PolvLach I-ast im S. ',,!. Kirov, Chair of Phys and ColLoid Chem),
150 coplies (KL, No 11, 1959, 116)

PROSKURYAKOVA, G.F.; SHVEYKINA, R.V.; CHERNAVINA, M.S.
Comparative characteristics of some most sensitive methods for
determining iodine in water. Izv.vys.ucheb.zav.;khim.i khim.tekh.
6 no.5:729-734 163. (VERA 16-12)
1. Sverdlovskiy sellskokhozyaystvennyy institut, kafedra khimii.

VEMIKOVSKAYI, N.V., kand.med.neak, SHVEYKO, I.I.
Effect of manganese on thyroid function. Trach.delo no.11:1207-1209
19158 (KIRA 12:1)
1. Xafedra obahchey gigiyeny (zav* - prof, P.I. Barannik) Kiyevskogo
meditsinskogo in8tituta.
(MANGANESE-FIffSIOLWICAL EFFECT)
(TMOID GLUM)

RODE, fl.i BARASHINA, A, LMRIN, V.,,, BUKCHIN, i., t-flROPOLISKAYA, S.,
starshiy PAVETKINA, L., rabotnik
Bank atallistles and methods for their menharazation. Den. i
kr6d, 20 rio~6-5~-63 Je '62. (YJRA l5t6)
Glalrnyy bukhgalter Latv-iyskoy respublikanskoy kontory
gc,sudlarst-7e,nnogo !~&rAa (for Rode). 2. Glaviiry bukhgaltzr Orlovskoy
oblastnoy 'Fontory gosudarstvennoge banka (for Barashina). 3. Glavnry
b-okhgalter Tadz~-L
,Icskoy respubilkariskoy kontory gosudarstvennogo
bank-a (fzr Lakeri-I. 4. Zamestite" g'-vanogo bukhgaltera K-",-skoy
ablastnoy kontory gosudarstvennogo An (for Mcchin".
4 .-
Khersonskaya cblastnaya kontor- z uJsirE tire nnt~ga bank& (for
6. Glawtaya truk-'rlg.:- Stavrcpol~!ikov
krayevoy kont~jry gcsudarzi'l-venn,-.~j7,c banka Shveykn, Favetkina).
(Ba-ak~ %zd
(Machine accounti-lw*j

SO V/179- 99- 3-9/4 5
AUTHORS: Bolutin, V. V., Gavrilov, Yu. V., Makarov, 13. P. arid
Shveyko, Yu. Yu. (Moscow)
TITLE. Non-linear Problems of Stability of Plane Panels at
High Supersonic Velocities (Nelineynyye zadachi
ustoychivosti ploskikh paneley pri bol'shikh
sverkhzvukovykh skorostyakh)
PERIODICAL: Izvestiya Akademii nauk, SSSR, Otdeleniye tekhnicheskikh
nauk, Mekhanika i mashinostroyeniye, 1959, Nr 3.
PP 59-64 (USSR)
ABSTRACT; The paper is a continuation of previous work (Refs 1 and 6).
The question of the stability of plates and shells,
exposed to a current of compressed gas, has so far been
discussed in terms of a linear representation (Refs 1-5).
For sonic flow and for moderate supersonic numbers M
this hypothesis is apparently completely justified.
However, for larger supersonic velocities, aerodynamic
nen-linearity becomes very appreciable. As was shown
by Bolotin (Ref 5), solutions different from the
unperturbed ones appear in aeroelastic problems, allowing
for aerodynamic non.-linearity, at velocities below the
Card 1/4 critical value. Among these solutions are some which are

SOV/179-59-3-9/45
Non-linear Pr--blems of Stability of Plane Panels at High Supersonic
Velocities
stable in relation to sufficiently sniall disturbances.
These solutions can be realised if the elastic system
which is subjected to the sub-critical velocity is
~(Ifft.ciently irregular. All real constructions have some
i 1 regular -i t _L es (def ec ts of manufac ture, deformations
arising trom aerodynamic heating, vibrations tinder the
influence of atmospheric turbulence and other non-
NL,ttionary factors, etc.), Thus in some cases, the
Qritical. veLocity deLermined by the linear aeroelastic
th~-ory is only a lower limit to the critical velocity for
real constructions, In the present paper, the edges of
the plate are assumed to be simply supported and
slascically restrained against axial displacements; the
prcssure on the plate is given by: 2x
-1 1 v X -1
P ~ P + (1)
c0 2 a
00
where p is the pressure of the unperturbed gas, v is
the nc-rmal component of surface velocity of the plate,
Card 2/4 a Qj is the velocity of sound in the unperturbed gas and

SOV/179-59-3-9/45
Non-linear Problems of Stability of Plane Panels at I-figi-I Supersonic
Velocities
x is the polytropy index. The component of load normal
to the plate is
e oh 29 lie + 6 p
3t2 0 tt
where if is the deflection, (10 is the density and
h the thickness of the plate, 9 is the damping coefficient
and A p is the excess pressure, which can be expressed
in terms of the Mach number and polytropy index by means
of Eq (1). The problem then reduces to the investigation
of the non-linear equation for the deflection of the
plate7 which contains q, subject to the boundary
conditions. One solution is expressed as a double sine
series and is dealt with both by an approximate
numerical method, and with the aid of an electronic
calculating machine. The results of the calculations
for particular cases are shown graphically (Figs 11, 5 and
-%rd 3/4 6), and indicate the existence of flutTer in the panel.
C
, Acknowledgments are expressed to N. I. Chelnokov

SOAr/17 9- 5 9- 3- 9/4 5
Non-linear Problems of Stability of Plane Panels at High Supersonic
V e In' fl i t J, es
and Yu. R. Shne%rder of the Mathematical Machine
Laboratory ~2-' , for participating in the calculations.
There are 6 figures and 9 references, 7 of which are
Soviet and 2 English.
SU'r3MITTED: Noveiiiber 18, 1998
Card it/it

88518
0. 1010 V179/60/000/006/0-10/036
1:03 1/,-113 5
\17111OR: Z;IIIVC!Yko, Yu . Yu. , (%I05COSO
T ITL;,: 'i'lle jtaj)iLity of j C.11-culir Cylindrical Shell in a
Gas Flow
il,':R 101) R; AL. Izvestiya -'kademii nauk -:~:ii?,Otdeleniye tekhnicheskikh
nauk, Melchanika i mashinostroyeniye, 1960, No. 6.
P;). 74-7-)
T "'.XT: The critical flutter velocity for an elastic cylinder
of finite length in a supersonic flow parallel to its axis is
determined. Piston theory is used in its asymptotic form. As an
auxiliary problem, the natural oscillations of a shell with
supported ends is considered. Then the displacements can be taken
in the form: mTZ:z ns
u(Z. S) = COS COS T)
mn
ns
V(Z' S) = B sin sin 7,
mn (1-7)
JT ns
S) = C mn sin m COS v
Card 1/5

38518
179/6o/ Ooo/o06/010/036
~'03 I/ El 35
The Stability of a Circular Cylindrical Shell in a Gas Flow
at = 1, 2...... n 0, 1, 2 ..... (1-7)
and the equation for the natura frequencies is obtained. The
characteristic vectors thus defined are used in the expressions
for the displacements in the general case. Substitution of these
expressions in the equations of motion leads to it system of
ordinary differential equations. Values of the Mach number for
which the trivial solution occurs in which the displacements vanish
identically are considered by introducing non-dimensional variables
and approximating in the differential equations. If the
tangential components of the inertia and friction forces can be
neglected, a single separable partial differential equation is
obtained. Using Galerkin's method, a system of ordinary equations
of the type already considered is derived. For large n (where
n is the number of waves in the circumferential direction) the
expressions for the frequencies given by the two solutions tend
to coincide. The same is true for the critical Mach numbers.
An equation for the value of n for which the Mach number
Card 2/3

88518
S/179/60/000/006/010/036
E031/EI35
The Stability of a Circular Cylindrical Shell.in a Gas Flow
attains its minimum value is given. The minimum Mach number
corresponds to n ',> 6. As the damping increases, n decreases
and the critical Mach number increases.
There are 5 figures and 9 references: 7 Soviet and 2 English.
SUBMITTED: June 17, 1960
Card 3/3

V.V.,, doktor t-~)Ikcbn.vatik, prof., MAKAROV, B.P., inz'h-., MISIMTKOV,
G.V., inzh.! SHVEYKO, Yu.Yu., inzh.
T
-Icing the asymptotic met~ip,4 172 ln-vestjgWng the spectrum of
natural frequencies of eLastic plates. Rasch.na, prochn. no.6:231-
-'5-3 560. (MIRA 14-1)
(16kastic plates and shells--Vibration)

3/124162/000/008/012/030
IOC,6/1242
AUTt1UR-. Shvey~q, Y p
U_u.
TITLE: Flutter of a circular cylindricr.-l shell
PERIODICAL: Heferativnyy zhurnall, Mekhanika, no.8, 1962, 36, abstract
BB221. (Tr. Konferentsl*i po teorii plastin i obolochek-,
1960. Kazan', 1961, 4,14-413) -
TUCT: An approximate exprez;sion is obt,-ined for the amplitude of
nonlinear vibration:3 of 3egment of freely supported cylindrical shell, with
a supersonic flow of gas flowing along a -eneritting line on one side of the
shell. The aerodynEmic lor-d-- are calcul,~.ted by the piston theory (third
approximation, neglecting the partial derivative of flexure with respect
to time). Some numerical date are given.
late. Cowflet'!
I I
Gard 1/1

29061
S/179/6i/ooo/oo4/oo3/ol9
EOSI/E-335
- i.
AUTHOR ShvevIco YU -Y-U' (Moscow)
TITLE T,!)e i.nfluonce of su-,)crsonic flo-,: of a ~;as on the loWer
C: ritical stress of a cylindrical panel
PERIODICAL Ahademiya nauk SSSR., Izvesj:iya, Otdc-leniye
tek-linicheskillch nauk. Mehliantka i i-ziashinostroyeniye~
no. 4 1961 pp 14 .. 19
TEXT. The equilibrium is consi-dered of a cylindrical panel
compressed in the direction of the generators and subjected to
the flow of a compressibLe gas, also parallel to the generators
(Fi,-., .1 Assuming that the Kirchoff-Love hypothesis applies,
t 11at t'ie deflection of the plate is comparable with the thick-
ness and t',
iat the sides of the panel are simply supported, the
differer)tial equations for the deformat:ion of the panel are
stated in terms of t'ie deflection and the stress function. and
t,,-Le boundary condita-ons are also stated.. The case is considered
in detail of a square panel (a b) ha-in~~ a radlus of
curvature R sucli that 0 k wh er e
0
Card 1/~-

P"Ie influence of
b2 a2
Rb Rh
29Ubl
S/179/61/000/oo,'i/005/019
E081/E335
5f) ;2
0 21"* 3
(2,1)
cand is Poi.5son s ratio The deflection is expressed in
tri~-onometric form and using Galerk:in's method 5olutions are
obtaxned correspondxng to one and two half-waves of deflection
along the Senerators. The lowest critical stress is determined
and is found to increase increasing flow -velocity.
Calculations are made for tae case 1: = 10 and the results are
show-1 gra-,Iiically The al-ebraic stabillt-%r
._)~ A , of the solutLon
is examined using GalerIzin-s Piet': id a-nd the Hurwitz Criterion
and the requirements for _~tabiiir-y are establis'lied
There are 2 figures tnd 3 Sovic;~ rcferences
SUBMT7PED April 11 1961
Card 2/~)

L 21113-65 EI-IP(m)/E*vlA(h)/UeIP(k)/El.4T(d)/VdT(1)/VvIT(in)/Z*iiii(d)/E';IA(l~)/EI.IP(W)/-
174P (V) 1FCS (k) Pd-i/pf-4/Peb AGD(f)-31AFTC(P) .. itl.
ACCESSION NRt AP5002598 S/0179/64/000/005/0112/0116"
A
UTHORt Shveyko, Yu* Yu. (Moscow)
--------------
_Jindrical shell in Itas flowt
TITLEs Stability of a liquid-filled Sy
SOURCEt AN SSSR. lavestLya, Makhanika i mashinoatroyl.~OLye, no.
1964, 112-116
TOPIC TAGSt cylindrical shall, cylindrical shell flutter, flutter
speed, shell flutter speed# minimum flutter speed
ABSTRACT: A closed circular cylindrical shell havLnga perfe'tly
rigid diaphragm at one end is placed in a supersonic stream of a,
compressible gas. The longitudinal axis of the sheillis parallel
to the gas flow and to the direction of the gravitational field., The
I- shell is partly filled with a perfect liquid; the stresses in~tha
shell caused by the hydrostatic pressure ar,s neglect~ed. The flutteri-I
of the shall is discussed and expressions,for deltermiaLng the.mLnimum
flutter speed are 'derived by using a series expausion~in coordinate
functions (which describe the natural-vibratLon modep of a nonloaded
shell fim vacuum) satisfying the given boundary conditions, and the
I _Ca.rd _ 1 /_ 2.
low MWENINIZZ

L 21113-65
ACCESSION NRs AP5002598
variational Galerkin me.thod, The flutter behavior of a shell com-n
pletely filled with liquid and of an empty shelV'~is Uriefly analyzed!!.:-,
and the increase in the minimum flutter speed caused.by liquid.im: i'~.:
pointed out, Some simplified approaches in determLning9th the first--:
approximation, the affect of the liquid on the flutter speed arecout,6.:7..~
lined* Orig, art. hams 25 equations.
ASSOCIATIONs none
SUBHITTEDs 300et6S
ENCLi 00 AS, ME.
NO REP SOVs 005
OTH%Rs 003 ATD
PRB$Ss 3164.
COrd
-2/2

e!T() V,i.Yu. (I-ioskva)
Stability of a cyll-ndrical .9hell w7lLh
f lc,,i-. ~T SSSR 'Melkh. i mashipostr. no. 2-1-16
8

_k_2g756_�& EWP(m)/EWA(h)/EWP(k)/-rWT(d)/EVIT(I)/Ev~,r(m)/ETC(m)-6/EWA(d)/EViP(w)/ EWP(v)
1' ACC NR: AP6011130--
CODE: UR/0424/66/000/001/0067/0073
EVIA(l) IJP(c) Sffffl
AUTHOR: Brusilovskiy, A. D. (Moscow); Mel'nikova, L. M. (,Moscow); Shveyko, Yu. Yu.
(Moscow)
ORG: none
TITLE: Vibration and stability of a cylindrical shell in a gas flow
SOURCE: Inzhenernyy zhurnal. Mekhanika tverdogo tela, no. 1, 1966, 67-73
TOPIC TAGS: cylindrical shell, shell flutter, flutter speed, shell vibration
ABSTRACT: The flutter af an elastic closed circular cylindrical shell of finite
length in a.supersoAiV`a`xiaI flow of a compressible gas of a certain undisturbed
velocity is investigated. An exact solution of the system of equations in displace-
ments which describes the disturbed motion of the shell, with all inertia forces
taken into account, is used in determining the flutter velocity of the gas flow and
associated vibration parameters. The expressions for aerodynamic component loads
acting on the shell are written by using the linear piston theory, and disregarding
the effects of the aerodynamic and structural damping, as well as the initial stresse
in the middle surface of the shell. The critical Mach numbers at which theflutter
occurs are determined, by analyzing the behavior of natural f requenices of the shell
in relation to the flow velocity; the corresponding frequencies of the shell are
determined by a numerical method in which a parameter is used which accounts for the
Card 1/2

L 20756-66
ACC NR-. AP6011130
rigidity of the shell and for aerodynamic quantities. The results of numerical cal-
culation of the minimum flutter velocities for a cylindrical shell with simply
supported and clamped faces are given and the effect6,Of support conditions,on the
sheil frequencies, vibration modes, and flutter speeds-are discussed and illustrated
by diagrams. Orig. art. has: 5 figures, I table, and 20 formulas. [VK]
SUB CODE: 20/ SUBM DATE: 02jul65/ ORIG REF: 008/ ATD PRESS:

Card 2/2

ACC INR: Aj?7:',04G76 SOURCE CODE: UR/0124/66/000/010/VO21/VG21
AT7:'F-t1(-):-1'- Yu. N. Shveyko, Yu. Yu.
TITLE: Vibrations and stability of two-laycr shells with flowing liquid in its
cavities
SOURCE: Ref. zh. -Mekhanika, Abs. 1OV160
REF SOURCE: Dokl. Nauchno-tekhn. konferentsii po itogam nauchno-issled.
rabot za 1964-19G5gg. Mosk. energ. in-t. Sekts. energomashinostroit. M. ,
1965, 103-118
TOPIC TAGS: elasticity theory, orthotropic shell, shell vibration, shell structure
stability, cylindric shell structure, shell stability
ABSTRACT: The problem of the stability and vibrations of a shell consisting of
two thin coaxial cylinders joined by a sufficiently large number of longitudinal
partitions is investigated. The cavities of the shell contain a liquid flowing at a
constant. velocity. The initial equations of the structurally orthotropic shell-are
derived as a result of a "smearing" operation. The pressure of a certain equiva
lent moving load of constant intensity is substituted for the pressure of the liquid
C.rd I / 2

ACC NR:
AR,700,1676
on the shell. A characteristic equation which serves to determine critical
velocities is devived through the application of Bubnov's variational method. Two
characteristic critical speeds are distinquished: buckling and flutter speed. The
expression for divergence rate is relatively simple. It is shown how to find the
critical flutter speed. For a specific example calculated on a computer, the F
divergence- rate proved to be lower than the flutter speed. There is a bibliography
o f 11 titles. [Translation of abstract] (DWI
SUB CODE: 13/
C.,d 2 2

S/219/62/054/olo/oo4/004
D296/D307
AUTHORs ShveykoV3kiy, A.B.
TITL-Is The removal of hair from the operative areas
on experimental animals
ill,"R I OD I 10,11L IAkademiya meditsinskikh nauk SSSR, Byulleten'
eksperimentallnoy biologii i meditsiny, v-54,
no. 10, 1962, 123 -
TZXT: The preparation of operative areas on experi-
mental animals is generally performed by mechanical means, such
as haircutting and shaving, preceded by an administration of mor-
phine. This procedure is lengthy and rarely complete. The author
proposes a chemical method of hair removal, based on an applica-
tion of heated 10 % aq. Na2S, over a period of 2 minutes. As soon
as the hair begins to disintegrate, the treated area is carefully
washed free of hair and the reagent, leaving a healthy, intact
patch of skin. Previous anaesthesia is not required. Histological
tests showed the hair roots and the epidermis to be fully unimpaired:
Card 112

S/219/6 2/054/01 o/oc4/oc4
The removal of hair D296/1)507
normal growth of hair resumes after the same period its after shaving.
Vumerous areas of skin were treated in this manner on 115 dogs, ob-
serving the animals over 40 - 90 days. No complications were detected.
The method has thus proved itself and allowed the author to prepare
the operative areas without resource to the mechanical treatment.
~-Abstractorls notez Essentially complete translation]
M
ASSOCIATION: Lsentralnaya nauchno-issledovatellskaya labora-
toriya Grodnenskogo meditsinskogo instituta
(Central Scientific Research Laboratory of the
Grodno Institute of Medicine)
6U.bMITTLD: September 22, 1961
Card 2/2

-.- -1 ~~
i .
"Accumulation of 7loisture in Frozen Ciround under 'L.i,,c Influence of a ThmperatLre deg-Lme,ll
Symposium on RegulaLion of tfte System of Hoad Founclations, Road and Hignway Fress, ~'Iloscow:
194t (V110-150).
(YeteoroloEiy-a i GidrolcCiya, illo 0 lov/Dec 1947)
SO: U-3216, 3 Apr 1953

.3EVIS*,"N-:r,, 1. A.
- -- - -- -- - -.-, - -.-, - ----- --------
Dissertation defeiided for the degree of Candidat.-, of Physimiiathematicai Sciences
at the joint 3cientific Council on Physicoraathe;-iatical and Technical Sciences;
Siberian 0'ranch -14",2
7 6, /--
"Riemannian 6paces Containing a Pole."
Vestnik Akad. Nauk , '.0. 4, 196), pp 119-145

SEVEYNOV, A.F.
Changes in the ribonucleoproteins in the epithelium of gastric
mucosa of dogs after generalized irradiation. Med. :Isd- 5 no.9:
30-33 S 160. (I'IIRA 13:12)
(RADIATION-PHYPIOLOGICAL EFFECT)
(STOMACH) (NUCILEOPROTEINS)

SHVLMi0vI_ AOF.--,-
Problem of the relationship of morphological changes in the
gastric mucosa of irradiated dogs to the changes in the
-IW14soproteins of the calls. Arkhpat. 22 no.3&42-47 t60.
(MMA l3tl2)
(RADIATION.-MSIOLDGICAL EFPWT)
(STOMACH) (NUCUMPRDTMNS)

SHVEYNOV, A.F. (Kursk, ul.K.harksa, 3)
Distribution of ribonucleoproteins in the cells of the epithelium of
the mucosa of the stomach in fasting and fed dogs. Arkh. anat. gist.
i embr. 40 no. 1:27-31 Ja 161. (MIRA 14:2)
1. Kafedra patologicheskoy anatomii (zaveduyushchiy - prof. A.S.
Brumberg) Kurskogo gosudarstvennogo meditainskogo instituta.
(FASTING) (NUCLEOPROTEINS) (STOMACH)

SHVFY"!r,',', F.
EP PU4, C"ntert
-%w] iilicl-ar R-11' conterit l:-.(' ri-!.ised gs rn: d' will -,?. -r'S'l),3 r
-8 Aw IIJ
TO,,
:3 Lf! 0 ti Aetrree ,jas a
On

VOLCHMO, I.G.; SHVEYSKIY, Ya.G.; TYRYKIN, A.I.
Enclosure for thawing frozen loads. Koks i khIm. n0.5:16-18
156. (Thawing) (VoIste heat) (SugAr boots) (Km 9.10)

C OU N P U3311
C AT,~~]r v arn. Anijiu0_.,j. Swine
JOUR. :RZBiol. , ~To- 13, 1958, 110. 59562
AUTIHIOR :Shveystis, Yu. YU.
Lith-u-a-mla-m Scientific Research Institute of*
PITLE :FXfeotiveness of Industrial Crossing of
Swine of the Lithuanian White-Breed Group
ORIG. PUB. :Byul. nauchno-tekhn. inforn. Lit. n.-i. in-t
zhivotnovodstva i veterinarti, 1957, No 2,**
A 93 T RA 1C T:Swine belonging to three groups (7 head's in
each) of the Lithuanian White breed group
wera crossed as follows: the control group
was mated to a boar of the same'breed, the
1st group to a boar with a White Short Ear
breed and the 2nd group to a Landras boar.
knimal Husbandry and Veterinary Medicine
33-36
CAaD-. 1/3
52

C A T Z~ 0 RY P a r m, Animals. Swine
JOUE. 4027Bial., 13, 1958, YO. r19r62
RUTHOR
INST .
TITLE
ORIG. PUB.
ABSTRACT The fertilitY of the swine of the 2rA group
cont'd. v-as higher by 36.21%o, the weight of hybrids
fit weaning was higher bY 7-4,"a% and the -mor-
tality before weaning was lower by 6% as com
pRred with the control group. In the process
of fattening, the pigs of the control group
achieved a live weight of 100 kg. after 140
days, those of the Ist groi~p after 133 days,
and those of the 2nd group after 120 days.
The average daily gain according to groups
V 3

Y
_J I SSR
U~
~_.:-TGRY Fax-i Animal s. Swine
0 U i-I RZBiol., No. 13, 1958, k1o. 59562
Aii-CHOa
17~T.
OR I G . PU B.
,2..,
A --j 3 T R A C vras: 502.5, r' 6.6 and 545 7 g., and the
cont d. slaughter outptit was 79-3: 7n.0 and 77.8;'0'.
As 8 raonths ol' aCe the index of compactness
(by groups) was 92.6, 96.3 and 93.1; the in-
dex of massiVeness was 170.7, 182.0 and 173.9.
The -hybrids of the 2nd F
,roup produced 31.2%
of internal fat, and the hybrids of the 1st
group had 16.9"'0' less abdominal fat compared
with swine of the control group.
3/3

Lis) ve. c-In-ri
of "'o ~~voup with bo- -o 0-11
Lan-, a a L.- T)e a anJ F3 o,.i- It-, I ct-~Jilc al foat-ou!of, of t~i- s ob tra in.- V 1 Tlz"-.-l s
sta'_-_a u Lil V. Yapsulmo), !,-10 cc-Dian
7v- -) 1

karid.
C-'J
.4 - a-_eo' fr-'r.
b, a a z u.1 t u! - a i
33~,

LEPP, R. (Lapp, Ralph E.J; RUBALISKIY,,B.G. Ltranslatorl; ROGINKO, Yu.Ya.
(translator]; SRV3YTS.BR, A.D. [translatorj; SOBOLZV, I.N..
general-mayor, red.; DEYEV, U.N., red.; KHOMYAKOV, A.D., tekhn.red.
(Atoms and people] Atomy i liudi. Pod red. I.N.Soboleva. Moskva,
Izd-vo inostr.lit-ry, 1959. 286 p. (MIRA 12:8)
(Atomic energy)

N,). 2,
0,-,L~rt~ June 11?5.'-. Uj,~cj-- c-ifi ed.
Df

TlLIZ, , Anatolly Alekoaridrovich; SIIVEYTSEH~ David V.1adimirovich;
ZktUBIIISKIY, Ye.A., red.
[Examination of labor disputes in the U.S.S.R.; a textbook on
the course:"Basic principles of the Soviet State and lav 0)
Rassmotrenie trudovykh sporov v SSSR; uchebnoe posobie po
kursu: Osnovy Sovetskogo Gosudarstva i prava. Moskva, Vses.
zaochrjr,, firiansovo-ekon. in-t, 1959. 22 p. (MIRA 15;2)
(Labor disputes)

6/0 4 a/62/0265/003/01 41015
B 1 02/B 104
V. F., and 6hveyt:jer. I. G.
C), the X-ray ezA~33ion spectrum for gejf- absorption
A tj zk I . !-,vestiya. Seriya fizicheskayn, v. 26,
422
f - the conti
are cOnSidf.--red 0 1 nUOUS
e~. ic
-j c ru m s e p -a r a t e 1
y . n the first caie, it is not
v--alues of fle aboori)tion coefficients. In
the int,-;njitj of the characteristic spectrum can be given
+ v; 4- "1 h
C'2 V -x 2V3 3172Vi + V3
C:' i7i.-* r~rljlrl V2)
i
X is th'~ -')'~,n,~!-.Ltion depth of electrons, and is the absorp-
n o f -,' 1 c i 3 n t .A :).-,_-.ct_Jca1 correction for self-absorption is demonstrat-
for t'no2 L '0-1rd and the L III spectrum of metallic Mo. The intensitie3
~d 2

SHVEYTSERI I.G.; SACHEM, V.P.; NIKIFOROV, I.Ya.
Sturcture of the energy levels of metallic molybdenun. Izv.AN
SSSR.Ser.fiz. 27 no.32319-321 Mr 163. (MIU 16:2)
1. Rostovskiy-na-Donu osudarstyennyy universitet.
(Molybdenial (Crystallography) (Quantum theory)

ACCESS101; NR; AP4039764
S/0048/64/028/005/0797/0800
AU711OR: Shveytser, 1. G. ; Nikif orov, 1. Ya. ; Sachenko, V. P.
TITLE: Concerning the energy spectrum of metallic niobium, geport, Seventh C*nf0-
rence on X-Ray Spectroscopy held in Yerevan 23 Sep - I Oct 19627
SOURCE: AN SSSR. Izvestiya. Seriya fizicheskaya, v.28, no.5, 1964, 797-900
TOPIC TAGS: x-ray spectrum, x-ray absorption, molybdenum, niobium. energy band
structure
ABSTRACT: In continuation of previous theoretical and experimental investigationg
of transition metals of the palladium group (I.G.Shveytser, V.P.Sachenko and I-Ya.
Nikilorov, Izv.AN SSSR.Ser.f iz.27.319,1963) the J, 2 emission and LIXI absorption
spectra of Me and Nb are compared. and their differences are interpreted in term&
of the energy level distributions in the metals as calculated in the orthogonal
plans wave approximation. The Mo spectra and energy level distribution are taken
from the earlier paper. The Kb emission spectrum was taken from work of U.I.Korsun-
skiy and Ya.Ye.Genkin (Izv.AN SSSR,Ser.fix.25,1028,1961) and the Nb L111 absorption
ipectrum, was measured for the occasion. The spectra of the two metals are rather
Card 1/3

ACCESSION MR: AP4038764
similar, but the following differences are noted: the 14~2 emission band of Mo is
both wider and more symmetric than that of Xb, and the first L111 absorption line
of Nb is wider than that of Mo and its maximum is located fartip-ar from the aboorp-
tion edge. Since no self-consistent wave functions are available for Nb. and since
orthogonalized Slater functions proved to be insufficiently accurate, the atomic
parameters of Kb required for the orthogonal plane wave calculation, namely the
Fourier components of the atomic potential, the orthogonality coefficients, and the
energy eigenvalues, were obtained by extrapolation from those of No. The extrapola-
tion )f the energy eigenvalues was performed with the aid of Moseley's law, that of
the orthogonality coefficients by means of Hartree's scale transformation of the
wave functions, and the Fourier components of the potential were extrapolated by
first calculating their dependence on the atomic number with the Fermi-Thomas model.
Thirteen orthogonal plane wave functions were employed in the calculation of the
energy levels; the method of calculation is described in more detail in the earlier
paper. Considerable differences were found between the level distributions in Mo
and Nb. In particular, the maximum density of d levels occurs near or below the For-
mi surface in Ito and considerably above it in Nb. The LjjI spectra of the two metala
are discussed in some detail in relation to the level distributions, and all the
differences noted above are successfully interpreted - in one case (the width of the
Card 2/3

ACCESSION NR: AP4038764
Nb L52 band) almost quantitatively. It is concluded that even Incomplete calcula-
tions of the energy structure of a solid can sometimes make it possible to inter-
pret x-ray spectra semiquantitatively. Orig.art.hast 3 formulas and 3 figures.
ASSOCIATION: Rostavakly-na-danu gosudarstvanny*y univ*rsltet (Rostov-tw-the-Daft
State University)
SUBMITMD: 00 DATE ACQ: 12Jun64 EXCL: 00
SUB CODE: OP NR REr SOV: 002 02=R:006
Cwd 3/3

ACCESSIO,% NR: AP4038774 S/0048/64/028/005/0834/0835
AUTHOR: Blokhin, M.A.; Demekhin. V.F.*. Shveytser, I.G.
TITLE: L Spectra of soma molybdenum compounds ffeport, Seventh Conference on X-Ray
Spectroscopy held in Yerevan 23 Sep to I Oct 19627
SOURCE: AN SSSR. Izvestiya. Seriya fizichaskaya, v.28, no.5, 1964, 834-835
TOPIC TAGS: x-ray spectrum, x-ray-absorption, molybdenum, molybdenum compound,
chemical bond
ABSTRACT: In order to obtain information concerning the extent to which electrons
in the Incomplete 4d shell of transition metals participate in chemical bonding, I
the LII and LIII absorption spectra and the 1482 emission bands of metallic molybde-
num, and Mo in M003, CalfoO4 and MOS2 were recorded. Although some of these spectra
have been previously reported, the results of different workers are not all in ag-
reement; moreover, the earlier spectra were not corrected for the width of the In-
ner level. The spectra were recorded photographically with a spectrometer having a
resolution of 12 GOO$ and the LIJI edge was observed with a second Instrument havire
halt this resolving power and employing an ionization chamber lor redording. The ob-
Card 1/2

ACCESSION XR: AP4038774
served spectra were corrected for the width of the inner level. the width of the Mo
LIJI level being assumed to be 1.76 eV. The corrected absorption curve for metallic
Uo did not break sharply; this indicates that the L11I level in in fact somewhat
wider than assumed. A gap between the emission and absorption was perceptible in the
insulators M003 and CaMoO4. The LIJI spectra were in good agreement with those ob-
tained by I.V.Borovskiy, X.P.Gurov,et al (Izv.AN SSSR,Ser.fiz.21.1401,1957). As the
valence increased, the absorption edge shifted toward shorter wavelongths.,This -
shift, which attained 3.4 eV for the LIII edge of CaMoO4. is ascribed to decreased
shielding of the inner portion of the atom by the valence electrons that become in-
volved in chemical bonds. A second sharp absorption line was observed in the LIXI
spectrum of CaMQ04 at 13 eV from the primary line. Such lines have been previously
observed in molybdenum compounds and are ascribed to transitions of 2p electrons to
the incomplete 4d shell. Orig.art.has: 3 figures and 1 table.
ASSOCIATION: Rostovskly-na-Donu gosudarstvanny*y universitot (Rostov-on-the-Don
State University)
SUBMITTED: 00
SUB CODE: OP
Card 212
DATi ACQ: 12Jun64
NR REP SOV& 008
EXCL: 00
OTHER:000

e v a
of rl c-, nLEE,
cc
o~,--!:ovok .-' ygo n-,- ~.:n` %,ers: i-men! C-mcn:-. S CV a

SHVEYTSER, V. (Schweizer, B.1; SKLAR, A.
Statistical metric spaces &rising from sets of random variables
in Euclidean n-space. Teor. veroiat. i ee prim. 7 no-4:456-465
162. (KRA 15:11)
1. The University of Arizona,
Technology, Chicago.
(Topology)
Tucson and Illinois Institute of
(Mathematical statistics)

. I
PILIPOVIGH, M.F., inzh.; RODENKO, K.V., inzh.; SIUMSER, V.D., inzh.
Specifications for boring and blastin-- operations. Bezop.truda v
prom. 3 no.7:29-31 JI 159. (MMIL 12 -. 11)
(Blasting)

RODENKO, K.V. (g. Vorkuta); SKVMSFa. V.D. (g. Varkuta); FILIPOVICH. M.P. (g,
-W Vorkuta)
Safety certification for boring and blasting operations in coal
mines. Ugol' 34 no.10:23 0 159. (MIRA 13:2)
(Coal mines and mining--Safet7 measures)

KICHAYEV. V,A. inzh.; SHVZYTSER,_V.D., iuzh.
I - - -
Use of rod baiting in the Pechora coal basin. Shakht.strol- 5 n0-4--
25-26 Ap '61. (AM 14-5)
1. Pechorskiy nauchno-issledovatellskiy ugolln~7 institut (for
Kichayev). 2. Shakhta no-40 Pechorskogo basseyna kombinata Vork-
ugoll (for Shveytser).
(Pechora Basin-Mine roof bolting) I

VDZNESENSKIY, Lev Aleksandrovich; VCjLKOV, Feliks Mikhaylovich;
SHVEYTSER. Ye.K. red.; PAVLOVA, A., tekhn. red.
[How to fulfill the work on tests and term papers in
economics; aid for the correspondence school students of
institutions of higher learning] Kak vypolnit' kontroll-
nuiu i kursovuiu raboty po politicheskoi ekonomii; posoble
studentam-zaochnikam VUZOV. Moskva, Gosizd-vo "Vysshaia
shkola," 1960. 28 p. (MIRA 16:7)
(Economics--Study and teaching)

KOSMUT, Filipp Petrovich, prof.; SHVEYTSM. Ye.K., red.; VOROMINA, R.K..
tekhn.rea.
(Economic low of the preferential growth of the production of the
means of production] Bkonomichaskii zakon preimushchostvennogo rosta
proizvodBtva sredstv proizvodstvla; materialy k lektsiiam po kursu
politicheBkoi ekonomii. Koskva, Gos.izd-vo wVysohais shkola," 1960.
70 P. (MIRA 13:10)
(3conomics)

GOLEVA, Yuliya Pavlovna; SHVEYTSER, Ye.K,.p red.; MURASHOVA) V.A.,, tekhn.
red.
[Loan capital and credit] Ssudnyi kapital i kredit. Moskva# Gos.
izd-vo "Vysshaia shkolao" 1961. 45 p (MIaA 14;12)
(Financei