SCIENTIFIC ABSTRACT RAUS, J. - RAUSHENBAKH, B.V.

• Document Type: CREST
• Collection: Scientific Abstracts
• Document Number (FOIA) /ESDN (CREST): CIA-RDP86-00513R001444320014-8
• Release Decision: RIF
• Original Classification: S
• Document Page Count: 100
• Document Creation Date: January 3, 2017
• Document Release Date: August 1, 2000
• Sequence Number: 14
• Publication Date: December 31, 1967
• Content Type: SCIENTIFIC ABSTRACT

LD,KF.; FUSKOVIC, D.; ~Usl il.-
lationship betwoen vJrrus multiplication and Inlerferm pro-

I -IIAUS, Jan; SIYK, Boh.umil, Dr.

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RAUSCH, J.; SZEGI, J.; MAGDA, Katalin; NAGY, Julia; BOGNAR, R.; SZABO. S.

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1213
AU-I 11011'
ll~ukhin, A. V_ and Raituticribakh, M. S.
Tll'(.F-, Ilom: marrow trjo~fmion for ircatment ordcprc~~d hemopowsts roUrswing irradiation
ITRIODICAL McAsWitskaya radwfogiyj, Y 7. na. 2, 196" 64-71
Ibc necrl~ify tarontinuc rmliation therapy in ra5cs ofmalignant neopLisnis forers one to Ittok for
offiwj~,nt r.ipi,fly-acting meani. Triniru~ion of hamslo~oui bone toarrow was tried
rlst .,(, J"gsaml monl,cy% At. induction ofacute radiition sickness. 90-93!1 ofcclis pfc-stfved their Ability
r-~r ru;t1wir diviiion and that hemepAciis sub-.cq"cntly improved markedly. This methad was then tried kin
40 patictiti ~% ho received 70 ttansrmions or homologous bone marrow. This Imatrit-trit had a ni-tried thcra-
pvtitic cirmi in too,( of the patient%, particularly amona those with the ituh3cute va. ictics o(h)Pj- and apti-itic
anciiiia. The authors conJudc, I%owi:vcr, that the mail number ofcases cit3minctlisinsufficient for definite
evaluation or itic thcrapeutic 01c.:9 or this method.
SUIINIITFED~ November 20. 1961
Card III

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rthus %vere treated with 5670
ta"Jum dich, t and the
fil
wtt
tus were exposed to rradiation from an UltmMmic
generator of 8W kc. frequency and an Intensity of 1-
%vatts/sq. cm. After irradiation a 0.5-mm. crystal of Ay-;'
NO; was placed in the cent r of the film and the formation of
Llesegang rings %vas Theno.'ofringslormedin24
firs. increased with Irradiation Intensity,
For each latta-
Sity; tile effect incre-ased asymptotically to a smiting value
%vids iucreasing duration of the irradladm.. The n-ilalts
sbow that the diffusion rate through the gelatim Is in~~
by ultrasonic wa 'yes tven though the gd stryAkinto is a*
broken down. Helbert Morawass-

MUSIL, Frantiock,; iUUSEA, Vladimir

~~Vera Aleksandroviia; VASILITEVA, O.S.
BLONSKAYA, liataliya Ivarlovna-,,W
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I I Abs Jour: Ref Zhur-Biol.j. No 1, 1958, 2150

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. A.
CHEPROOV. S.Y., nostavitall; YUZAIPOVICH. Ye.j.. sont&vitoll,- RATJS . T.,L.

7
bakh B V On a @mark by PAylefgh con-
'-12 R..sh-Al
kc:4-
d
(In R--Ia N DktW1 A
i
-
o
com
ng
l
Mauk &~~R (M.S.) 91,4,740-752, Aug. 1953.
-
The values d q for houtm o0cillations are C14 a circle witb,racrm
ng nor de
Author considers neutral caelliations, neither Incioasi and position of centerdetenalned by ji, and vi.

creasing In amplitude, of a gaseous system containing an Inter- For a system gonemung HIN WIN tones, We, AIC:50,
face where beat In released. For neutral oscillations, presmre..
. and WIMP, (EIC)*%?-O, neutral isciffallono an impossible
~
on either side of the Interface.
In 90, out of phase with velocity only with beat addition in the smoil quadrAAL
A neutral Ong,
lie assumes small amplitude linear oscillations and Iscutral I)ir- lation is pooalu with boat addition In the third quadrant.- this
he
transfer of gas across the following
tly conflicts with Rayleigh's byjwtheole that hes,
t must
general equations be added 16 phase with the pressure to produce driving. When

I the mean raW of now is so he equation airees wM 1141olgh's
ps - allp, + any, +
anq
hvot6lx~- For a 'mean rated flow'ilrestar than Sao, negiect
v
- amp, + duvi + a
j UCI
of kinetic encrgy by Rayleigh is Ind1614 do eause.of the:
discrepa Y.

whe I and 2 refer to before and aftei
re
'
cle Lu- bet I
rull! Atik UrgA.
Systoln, P
are ionstants which depend on the parameters a W system and the, P1 Ts Wistem shuti-to su ,ch an extent, that he q
Is bacillatIng pressure, v Ix oscillating velocity, and q Is ovillating, exist
a giving neutral oecillatloaa.~- (R"w a note: Au r ha
beat release.

The dot products ps - Y, and ps - vt are both zero. Thus, takhou,
not p4ayedthat Rayleigh's hypotheols is not sufficlont by It4elf,
providing the heat Pnew: to properly: partitioned between ihe
Pi as the x-axis and q, as the y-alxij, the scalar-product of the I. Ad. of the: Wedsc,) W.AL Denals,
above equations becomes
Apig. + B", + Qq., + 9 1) + Dp1j +.Svt m 0
4e
r

On the Problem Cencerning the Longitudinal Stability of an
I'dreraft In Unfavorable Flight Conditions," by Tiberiu Hacker,
cetari mes.
Ludii I cer apl., vol 6 NO 3 1955, pp 2.49-
(from Referativ-nyy Zhurnal Mekhanika, No 1, Jan 57, Abstract
1o 2
1
96) by D, V. Raushenbakh)
The article discusses the longitudinal disturbed motion of an air--
craft on the supposition that the undisturbed motion is rectilinear and.,
horizontal. A dimensionless system of equations.is introduced, in
Uhiah
the unit of velocity is the =ximn flying speed. In the case when the
undisturbed motion of the airplane'is set, the minimum flying speed is,-
the most disadvantageous from the viewpoint of the short periodic stage .
of the disturbed motion of the airplane.
Adequate conditions of stability occur for cases of acceleration a6d,.-'
.:deceleration of the tnidisturbed motion. It is shown.that duringshort,
periodic disturbed notion a statically stable airplane can lose dynami c
:Stability only with slow undisturbed motion.
A de-ternination,of:the critical value of the acceleration is give
for the latter case. In addition, the disturbance of the axigle of atti
ek
and the angular velocity.of pitching are.giyen. Ile dar4)ing velocity of,
some major functlons,~uhich limit,from abo t ant of,time~.the
ve,. a any MOM
a~mplitudes_of the above-indicated.disturbances is.also :round.!' It was
shown that.the da -m-pixig 46locity of the major functl on* In general- &6":
with tl~e increase~of-l ,th -'tl speed. (U

20-2-16/62
I Rau~3he bakh, 3.VP
n
T I!Lil ls~, On Energy Sources at the Thermal Excitation of Sound
(Ob istochnikakh eneigii pri termicheskom vozbuzhden11 zvuka)
YER I ODI CAL s Doklady Akadcm ii Nauk SSSR, 1957, Vol. 115, Nr 2, pp. 256 258
:(U,90R)
STRAM The author th ks that the,problem of the energy source on the
in
occauion of the thermal excitation of sound in a moving gas is in
various -aorks incorretly solved. The authqr puts down the equation
..of the enerey flow in the form E v212) + 9 ve T + pv. In
thio connectio n 9 signifies the density of the gaev, p - 'the
pressure, v -.the velocity of flow c T the internal energy.
V
The first.two terms of the sum descr be the transfer of en e rgy
i
by the nass flowand the last term.of t1v sum describes the ~trans-
fer of energy by means of pressure. The last term pv:is most im.~.
portant. An immovable domain E of the heat conductor be.bounded
by two control surfaces which stand vertical to the axis of~the
here-examined unidimensional surface. This domain 2 have g small
extension as compared.to the wave length of the oscillations to ~be
1/3 excited and therefore the hypothesis of the principle of immobili-

On Energy Sources at the Thermal Excitation of Sound
tY Can be applied to the processes taking place wi thin C,
author compares the onergy flows pv on the planes bounding the
donain .57 and he poses the problem of the amount of enera which
is emitted by this domain of the heat conductor. The source or,
this energy is also treated here. First the laws of conservation
.for this energy are separately written down for the flow element
in the reference system moved together with it and for the center
of gravity of this systems The flow of energy pv,emitted by the
domain Z is equal to p v - p v and thus consists of-two terms
2 2 1 2
of a sum& The first one is connected with the addition of heat
and with.the modification of the flow of the internal energy, the
second term is connected with the mechanical energy to be supplied
and with the modification of the flow of the kitatic energy. The
assumption of theflow paramters on the boundaries of the domain
is not sufficient* Then it is assumed that the quantities p.and v
have the components (Sp and Sv which change harmonically with
progressing time. An expression is then derived for the mean
accoustic energy emitted by the domain There are 3 referenc'-
.Card 2/3, es, I of which is'Slavic.

RAT31LEIMAY01, B. V. (IAQS,-Ow)

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23U83
S1112316,11000100910261627
A004/A104
AU 'MOR Rausheribakh, B, V.
T 1171U.- lheor4tlcal aralysis of vibrAting ~:ombustion of a gas mixture in a
PERT)DICAL., Re f 9ratlivryy zhurnal, Mashinostroyenlye, no. 91 1961, 20, abstract
gi'.66. (V 5b. '3-e Vses. soveshchaniye po teorii goreniya. T. I.".
MO
scow, !960,
Ta"T .-h ombustion is
Tk-4s ,heo--etleal solu"on of e problem of vibrating.c
divided intlo 2 parts. the dA-stription of the acoustic properties and'the deacrip-
tion of the combustion %one. The second problem Is solved by a:n analysis of the
stab!-Iity of the flat.d -tsion pl-,Lne between the cold gas and the combustion
proiu---ts. From the Eu' luation and the contlnuity in a linearized form the
frequency, ampl i ~U - ar. er parameters forthe vibratirg combustion in a 'tube
de
are found, With tne aid ~. the,obtained equations the author investigates the,,.
cite vibrating combustion in tubeg closed at~
zones In wh'1' ch It- is possible to ex,
end. in 6ombustion are
one. It is ahcwn thiat zones. of stable and unstable vibrat g
ob~lained solution is con-f"Imed. by tests.
alternatIng IM tubez,;. Tte! 6 . 1. Barak y
[AbvtractorTs Complete ~trenslatlon]
gard

D.V., t!-Ocr md.

t
's)--2/EWT(m) r-
32971 65 '-EPA/ 1VEW
W/N7MD
s/booo/6 5/01CO;-~
ACCESSION NR. Azoo4o8o
c'to'r.-o'f tecb c ac ences
AUTHOR: Paushenbakh, air i,
B. Ve Do
.............
TITLE: Introducto word on, Burni~g in, Vai-ious Type-`df O)aftation rk
ry
khnl aya konf6re'h*tsiy'
SOURCE: Vaesoyuznaya nauohno-te ichesk a po problemie'Lvibiatsi~;
:~t onnogo i pullsatsionnogo goreniy~. isi, 1961'. Ti~dy. Moscow i Sektor'nauc 0-;.:,:
IM
tekhn.-inform. GIAP9 1:9621 5-~
7
an coMbustioivthe ry
TOPIC TAGS; combustion alysis ustion'reseaich'L 0 pul u6n
qombuction- vibration combustion, scientif io'conference
'd
it inti i
ABSTRACT: s.paper,was wr ten as o uct on to the'o tiansiict onS bf,th6
of L
I -11nign acientific and'Techiiibal~Corifekence:on~the Problem t
Pulsa. on:and,
Vibration Combustion This is the first conference 3evoted toproblems-.o
tion combustion in industrial ins'tallations.~ Therefore most of the papers are
:~'Many Of,L with
the nature of.preliminary reportell the papers have subj ecti; in common; . ......
L
one another, therefore it was 'L n6cessary to a4oid.repetition." A survey of the
h cate that:not"all, ~which o
reports whic were presentedindi brgahii~tions are d i~g
vibration combu e ne tru-M
useful work on stion have 'th cesiary ins lents More- iban half

-----------
3Ml-'( :6
Istion'.''.:::~Most ... 0" t-:
SU~: CODE FPI GO'

40'
-L 1A&LIf7-63
ACCESSION NR AM050o
.
TABLE OF CONTENTS Cabridged3v
i
_...
Foreword
)Symbols' 6'
jIntroduction -10
Ch. Io :Some 'problems. of ;the .--thermodynamics -of - combustion- chimbers
'Ch.,Il.: Fuel mixing
Ch. III, Ignition and-combustio'n of homd eneoua"fuel'air sixturea:in .
laminar flow 175
Cho Ivi, ..Turbulence of~air.flows 210
'i
iii'
l
C
V
C
b
t
6
u
t
r
i
t
b
nt fl
f h
ii
.
2
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om
u
ow
h.
.
us
ion o
0m
m
x
u
e
oua f
es
n
ur
ge
~ 5.5.

"'Y
Ch., VIi Vibration regimes of
:coinbustion
,
Ch. VII. Flame stabilization in f2:o1i,'.of,_a" fuel mixtur
Ch. VIII..:Combustion of*fuel-a:Lr iikturee behind-a"body with poor flow -'-4031
i
lla of a'-c~mbuistilon chamber-and nozzle' --too; 440
Ch.:IX. Cooling thewa

SUB CODEs PR r64,.,, IR REr SOV%:112
SUBMI TED: 2OKa
OTM: .079

Card :2/2

L 1,14974-66 - EWF(m) -2/EWT UWE-W-T AST
ACC NRI AP601959U
SOURCE CODEs UR/0293/66/013,1/OG5/0367/03771
A
M
MORS: Legoatayev, V. F.; Rauehenbakh, B. V.
I~ORG: none
TITLE: Single oxis orientation system of the space ship~voqtok'relative to the
sun
SOURCE: Koomichookiye isoledovaniye,.v. 4p no. 39 1966, 367-377
TOPIC TAGS: satellitop orbit apace flightp satellite orientation, Wroul.cope
ABSTRACT: The solar orientation system used in the manned-satellite series "Vontok"
is discussed.. This orientation system consists of a photoelectric (s.olar) sensort
three two-atage gyroscopes# a logic networkp and small compressed air reaction jets.
Each component of the system is discussed in some detail. It is shown that the three,
relay type signals which indicate the illuminated and dark fields-of-~view of the solar
aenbor constitute a very simple system. The two-stage eyroscopesServe to damp the
angular motion of the satellite along each axis. The angular velocity.nensor placed-'.
on, the pitch axis has two regimes, whereas the eensor placed an the yaw axis.haa only.,
one* The logic for orienting the apace ship relati,7e to thwam is discussed in
detail#firat for pitching motion and nexti for the yawing iotion. The dynamics of
these'two motions are analyzed, leading to the eqxmitions for the angular displacement',
:8 which for yaw give" S+ZA+k% .+I a*La6+b Stu,,aN4.,l