SCIENTIFIC ABSTRACT NOVOSELOV, V. S. - NOVOSELOVA,, A. I.

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• Collection: Scientific Abstracts
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• Original Classification: S
• Document Page Count: 100
• Document Creation Date: November 2, 2016
• Document Release Date: August 23, 2000
• Sequence Number: 12
• Publication Date: December 31, 1967
• Content Type: SCIENTIFIC ABSTRACT

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ACC-ESSION NR. AP5002093 S/O*--461-'64/007/()06/0096/0104
AUTHOR. Novoselov" V. S.
o?5
"r ITL E ~Engineering calculation of optimal tihock absorption for measuring 46
mochanitims of shockproof instruments
SOURCE; IVt3Z, Priborostroyeniye, v. 7, no. 6, 1964, 98-104
TOPIG TAGS.- shock. absorption, 9-hoq!~2roof instrument_ 0
ABSTRACT. This is a continuation of a nurA,bey of eavIier author's' works- on the
SL.b~-ct. The calculation of optimal shof-It absorption is based on the
ilzy of coincidence of zla'ku~-'J and elastic
r; the range involved :6 j:
a'; r" 1 ~1: _r P at. lj~:
.-4". S r
at aPoin o~~ ;d4sa,

L 25,t4g-65
ACCESSION NR: AP50OZO93
h is the thickness of the shock absorber; & is a coefficient close to 1. Thus, an
absorber fhat has minimum stiffness and thlcknesR is optimaL The application of
r~-~(-Iihod to two typicall engineeritig problems set forth, Orig, art. has:
4~; v,,,res and 12 ;crrnulas.
T
eningradskiy gosudar6fvennyy univer-r-ilc-t (Leningrad State
e.- S L t V)
-'3-. ~.Jj -1-1 E;0: 160ct63 ENGL: 100 SUB CODE: IE
:;f- 4.F-F L'~OV: 00.1 OTHER: ~100

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ACCESSTON V OR : AT5001342 S 2 7 0 364 0 00 2 3 0 16 9 0 L 8
A Ul"HO R - Novoselov, V. S.
r 1 T LE. Cptimal spatial maneuver for entry (if a j~,t-propelled spacecraft into
,i zirculor orbit
LM LI-,- I-ad . Un t Ve 1-q P t . U01 0 r-, vve 7ap t 32 3. 1116/4, SeHva
ma "eciia tAr-hesk! kit nauk, no. 37, Tr,,jtl-; i-
_pagt!~raft.ortj celestfat mecbanica. spocecra" propul-
TO P I C TA GS : spaceship, a
Sion
BSTRACT: In Section I of this theoretical paper author formulates t.be prob-
6,~terTnlxiirg the optLtntal Spatial man,~,uver f,)r pilAcem~n-,!~ -f a Jet-propelled
spacecraft inLijr a-pAr"culjar cf-rctil,it -(0- ~ir%~~-:-' r, ,;yTmiietrical cen-
ttaj, body in apfic"e, expen4ing a minimal quantity of mas5, ;:,.,iE Possir-ion of the
~1 rt. Ir determined by spherlcal coord .1na te6 (r-1' y, assming a parti-
see g.
c, orbit with radius R 1q princ.1-pzI rezdfrg plane I of
The di,;Law-e ',c 11v renter C-f "lie body at t h 0.
j 0 f t' e maneuve 5 -11, i~-! n o 1, e; C L rcc!- 1 )r.C h c
-I Ia 47,is of the craft.
,;R(. '1hr,!9 L N is aostimed to coiric Lee url

T ?/ OF'--)-6r
ACCESSICN NR: AT5001342
Turni:fzzg~ toith- -atv auxillary jets engine of low
thrust or by other methods. Direction of the jet thrust is given by two angles:
V~5 !~~e angle between N and the radius vector andy is the angle measured around
i from the paratlel L l) thle ol~ n! in 1 i i - c, t It) I iH t h P gr e -i t
r;' i e 1~ ,,hoae pLane passes chrough N_ it in !Ah"if, iAif: 1~1~'eriwl moLion of
r the conibwstion chtimber f !;r- it -,te~idy st~ite, r-
P Sec' [cr, 2, after 11.3 V L 11 1; P.'!! dTA 2 er i r P e c. r r e s -
rmitias . the auther iefioc., t i 0 n s
Y -.11 w;111il lis; ~b& r~-cl(et -om tie
n. Y t 0f the t 11 r us
-ite to a circuLar orbit 4 r I,
'!Pen,
-ckL~t f,nz'"ne does noz dievelop
f ~e 1. , In Section 3, Lt is s i. ~;) ~. ~ ! ~i~ i - I
t; ons grPater than g'. Th,~ ;u I - h- r pr e -, e - t ~ -i sol,iriort for finding the
glow tra-nsfer of the e:raft frore. tlie same 3tite a,; in Secrion 2 to a par-
c~ rcu'ar orbit with radius R. In Sectft,-~i ty is ass,nned thpt the trans-
-hi craft to a circular orbLt is quite raptil ~ir) Lliac Lerms of the order
-'-ir4n,, the maneuvering cime do not att_ain large. valoes, It is
t';rar, a rapid regime of contr,~,l in which thrunt constderably exceeds the force
ton aP4 in which the Coriolis force of the internal motion in the com-
C (Imber can a t t a in a cons ider ab 1, ~3 vA Lue w i be oip t I ma 1 fo r cong t ant
I ne, I tnat ion o f thrus t to the o v. I ve r tind r a I t 1, 1. 1 f the.

ACCESSION MR: AT5001342
acceleration developed by the rocket engine is limited to a particular value,
art! approximate optimal regimes of programmed thrust, Including sectors
jet acceleration. Analytical expressions and examples are presented
f `a.3eg considered, Orig. art. 1i-t;4, 55 form,il-aFi ajif,i 1. fjgur!r~.
y a ~ ~~,jc - - ~ -, - - - -! L 1 v r 9 t-vennop P
As t rovomi ch-eB a
!:a t r o n o r , J c a 1, c, b s r:, rv i t r - - r r a d r. r. I v r C; 1 t-
(7 OE- FV
00
S-)V: 0011- t)/.
'14

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23-o5
T
S/ 3/65/WO/001/0I,'O./OI2O
A-P50D5763 004
AUTEOP.- Novooelov, V. S.
TITLE. TIN-ory of approximate solution of variational problems and its application
to thp study of moti-on of a Point of variable mass
SOMCM; L4~,n t. Vestnik. Seriya matematiki, mekhaniki i
-020
IOPIC TAGS: calculus of viaristions, optimal control
ABSTRAM Theorem 1. Suppose a control uk is expressed in terms of auxiliary
% 1.
controls Yk* In the Euler equations, the conditions of traneversality and the
equations obtained in minim'izing the Pontryagin function, terms of order F-m-1axe
d~rnpped, and in the oonstraint equations and the boundary conditigno, terms of order
6 Bi- are dropped i : Thow- the evror of , the optiroa-1. value of . the fimotional in the
oontrols Ykhas order Sm for m > 2. Theorem 2. Suppose the controls UkI f Cyr
which finite bounds ithl -de UAr < 142) U"' = cor,-Si u~, = const,
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L 29123-65
AC~CSSIOTI XR: AP5005783
are gii~enj om be involved on4 lineariy in the functional being minimized and in
the related motion. In the Ealer equations, the condi-
tion& of transversality, and in the corresponding equations obtained in maximizing
M-I
H, terms of order 4 are dropped, and in the constraint equations and the bound-
m
jw7~ omdktionpy- termq-of-order-4. _are, dr9j3,p9d. Then the error of the optimal value A
'the
.0
f the-
t 2 ~.-baaid of, eW djvemd~' he. -g
the- field of cen a
~Luthor treats coplanar motion of a point of variable mass in ir 1
farce. These two theorems simplify the construction of appro-timate solutions of
-~ar:ational prollems. The author determines approximate optimal trajectories of the
Orig. art, has: 2 figures and 45 formulae.
Motion of a point of variable mass.
Z
ASSOMIT . .. ..
..zon
SUMUTTEM.- MICL. 00 SUB COM MA
M
NO- r---~F SOV i002 OTHE"R 1002
21"?

.3, 1
3,1,2.00
89506
311043/60/000/001/012/014
0 111/ C 333
AUTHOR; movoselov, V. S.
TITLEs lotions of mechanic systems with bindings depending
on the variation of the masses
PERIODICAL& Leningrad. Universitet. Vestnik. Seriya matematiki,
zekhaniki i astronomii, no. 1, 1960, 132-141
TZXTs The author considers the set up of equations of motion of holo-
nomous or nonholonomous systems with variable masses, where he
assumes that the bindings depend on the mass variation.
Assume that a system has lolonomous ideal bindings which depend
on the Cartesian coordinatest time and masses. The general equation
of the mechanics of variable masses
(M W - r - Tj ) Sit - 0
j J j i
where the reaction forces consist of impulse forces, Coriolis forces
and forces depending on the relative accelerations, attains the formt
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Notions of mechanic systems
2v 2
(& . j -
i-1 j 2 aii
895W
S/043/60/000/001/012/014
. . . 0 111/ 0 333
'!Q - 0
where are the generalized reaction forces.
The prime means# that, for calculating the generalized forces, the
virtual work must be considered which is caused by the dependence
of the bindings on the mass variations. From this one obtains the
Lagrange equations
d 2T aT G
dt 34i a qi I
where the additional generalized forces are
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Notions of meohanio systems a Ili/ C 333
y L( dmj ,J) 3r, 2 qmj
GI 'Ej , __:._ a
dt Sq:L 2 4aqi
As an example the author considers a three-wheeled car which rolls
on a coarse horizontal plane, and the wheels of which consist of un-
winding absolutely flexible strips.
Then the author considers systems with holonomeous and nonholonomous
bindings.
An example with variable mass and nonlinear nonholonomous bindings
depending on it is given.
The author mentionst N. G. Chetayev, S. A. J"haplygin and P. V. Voronets.
There are 5 Soviet-bloc references.
SUBMITTED: October 27, 1958
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69756
S/043/60/000/ 007/011
ATJTHORs NovosLIO!, V'S.
TITLEs The Fall of a Ball Drop Dtiring Evaporation or Condensation.
Vapour on -its Surf6c-e
PERIODICAL& Vestnik Leningradskogo universiteta, Seriya matematiki,
mekhaniki i astranomi.1, 1960, No.2j pp 116-119
TEXTt The author considers the.slow and the quick.fall of a s
pherical drop
in a resting atmosphere with corte~,Ae=tion of the condensation or evaporatio'n
on the surface of the drop. For the slow fall the velocity of condensation
is described by the Maxwell law (Ref.2):
(1, dm ekr,
at -
where a is the mass of the drop, r the radius of the drop, k=const. and
e = +1 for condensation, e - -1 for evaporation. For the quick fall the
result of Frdssling (Ref.3)
7'
(2) e p r Y3-r
dt -
is used, where p=const 0 and Y is the velocity of the drop. For a small v
the air resistance is put --IY,'rr27 and for a large v it is put - plCr2v2. For
both casee the au-thor gives motion equations and integrates them approximately.
Thexaare 4 referenceBs 2 Soviet and 2 German.
SUBMITTEDt April 10, 1959
Gard 1/1

MOVOSRIDT, V.S.
Malling of a soarical drop with evaporation, from and com-
densatlon on Its surface. Test.Uff 15 no-7:116-119 160.
(Drops) OM& 13:4)

8/103/60/021/06/02/010'
B012/B054
AUTEEOR% Novosolov, V. S. (Leningrad)
TITLE# Investigation of the Probable Stability by the Example of
Automatic Control of Airplane Course
PHRIODICALs Avtomatika, i telemekhanike, 1960, Vol. 21, No. 6,
pp. 666 - 6T3
TEXT; It to assumed that the notion of an automatic control or regulating
system is determined by differential equations with random parameters and
random disturbing forces which, an a wholeg are designatod an random
factors. If these random factors are missing, the motion of the system is
called,undisturbed. Definition* are suggested for the probable stability,
i.e., for the little and for the very probable stability of undisturbed
notion. The term of llttle~probablo stability in a variant and a certain
generalization of stability determination with respect to the upper
dispersion.limits (Rof. 1). The definition of very probable stability is
connected with the term given in the papers (Refs. 2, 3, 4, 5). Three
theoreme are set up and confirmed. The explanations given are illustrated
Card 1/2

Investigation of the ProblLble Stability by tile S/103/60/021/06/02/016
Example of Automatic Control of Airplane Course B012/B054
by an exaapl* of automatic control of airplane course with the aid of an
autopilot at a constant speed of the servomotor. The inequality of
Chebyehey and functions of A. X. Lyspunov (Hof. 9) are nentioned, There
are 14 r0orencess 13 Soviet and I German.
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14.4too C Ill/ 0 333
AUMORs Novosolov, V. S. (Leningrad)
TITLEs Notion of Nonlinear Gyroscopic Systems
PERIODICALs Prikladnaya matematika i mokhanikag 19609 Vol. 24, No. 6,
PP. 1030-1036
TEXTs In his former paper (Ref.1) the author has shown how to obtain
in the general case the rigorous equations of motion of a mechanic
system with gyroscopes with the aid of the Routh-function
(1.2) R r Ck(H + hk) a aJk4J + a0 k) + T' (11 5~'Ihk)
F., ( J ;.
C was the axial moment of inertia of the k-th gyroscope, r the
itr of gyroscopes, H a sufficiently large constant h. - hk(t)l a7m
the cosine of the angle between the veatir of the angular velocity
j and the axis of the k-th gyroscope, a the projection of the
Ngular velocity of the bass on the axisoof the k-th gyroscope,
Tlithe kinetic energy of the absolute motion of the elements of
the suspensions,-of the casings, of the motors ate. Under application
of the precession approximation it is put T* - 0.
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0 Ill/ C 333
Notion of Nonlinear Gyroscopic Systems
In the present paper the author gives asymptotic estimations which
allow for finite variations of the position coordinates and velocities
to state how far the procession approximation is satisfactory. The
author particularly statess
If the base of the gyroscopic system is fixed, and if the
generalized forces of the absolute motion only contain terms of
order zero with respect to H, then it holds J
(2.6) jq i - gil - 0.(H- 1) ,
where qi and g correspond to the rigorous and to the approximative
solution with'14 - 0. If the rigorous solution is iought in the form
(H-1t) + xi(Ht)
(2.1) qi - qjI
then estimations of the kind x zil . 0(H-2), O(H-1)9
O(H-1) can be givent where the z i satisfy the same
initial conditions as x i and certain simpler equations. In particular:
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~0~634h ]j'X
v is the north omponent of the velocity of the bass, R
Jdius of the ea'rothgw angular velocity of the earth# 9 and Y
ftlerian'-an I a (measured from the local vertical and the parallel
to.the east *
The author thanks A. Yu. ishlinakiy and Ya. ff. Roytenberg for
advices.
C;ard 3/4
Xotion of Nonlinear Gyroscopic Systems
If a quickly rotating gyroscope of variable mass (Ref-3) is deflected
from the vertical position by the angle '19 1 then in the variables
0 andIF it oarr'ies out oscillations arouna the approximative solu-
tion defined by the precessiol theory$ the amplitude of these
oscillations has the order H_ and the frequency has the order H.
If the bass is movable and if the generalized forces can have the or-
der of H',~then the approximative solution (T* - 0) reproduces correct-
ly the gyroscopic motion in the coordinates 9 andf up to terms of
order 019 where
01 - max 11-1, 0 ( VN 2, O(C42) 0 0V (a 1 0-v32gi 1 0
_V I
(-LR+ CR(H+h),.,?$

3/040/60/024/006/008/024
0 Ill/ C 333
Notion of Nonlinear Gyroscopic Systems
There are 3 Soviet references.
CAbstraottir's notes (Ref.1) is a paper of the author in Priklad~%&Y& Ix
matematika-i makhanikag 19599 Vol. 23, No- 51 (Ref.3) is a paper
of the author in Izv. AN BSSR OTRI 19589 No- Ill.
SUMTTEDs. March 59 1960
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Ito% 17M 1144
D274P%3~02
AUTHORt Novosel S...-
TME: Extremum property of Buler-Lagrange principle in
nonholonomic mechanics
FMIODICALt Leningrad. Universitet. Vestnik. Seriya matematikil
mekhaniki. i astronomiip no. 4P 1961t 138 - 144
TEXTt-It is shown that for a mechanical system with nonholonomic
constraints of Chetayev typet
'Pk (qjP 4it t).= 09 !F-k 64, 00 (1.1)
and.variation defined by Voronetep
A 6cLi I 64r = At 6ji(i lt 29 06-9 8) 6?k 09 (1.2)
the functional of the Euler-Lagrange principle has a minimum on

290293/043/61/GOU/004/UO7/008
Extremum property of D274/D302
the actual trajectory. In such a formulationg the Ruler-Lagrange
principle is expressed by
t
2T dt = 09 Aqj. t = Aqi t At t = 0. (1-3)
2 1
If the system motion is considered as the motion of a point in s-
dimensional spadeq then (193) is written as the Jacobi integral:
(1-5)
where h is the energy integral and II the potential energy. After a
change,of variables one obtainst
(1.6)
Wz=' ..,d.
. .. . . . qi fj qj0
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Extremum property,of D274/D302
Iaochronous variation with fixed 41 is denoted by 61; such a varia-
tion is called Jacobi's variational method. The constraints are
assumed explicitly time-independent:
Pk(qip qj) = Oo (1-7)
The extremuih problem for the functional (1.6) reduces to that of .
the Hamilton-Ostrogradakiy.principle with a more complex Lagrangian
1,. For the second variation of the functional (1.6) one obtains:
8!W= 9,'dq, + 0 (q, - qely.
v, 1-2
where the quadratic form FB is positive definite. Hence the theo-
rem is proved that for mechanical systems with homogeneous statio-
nary constraints (1.1) and variation (1.2)p the functional W has a
minimum on the actual trajectory# for small domains of integration.
In the case of large domains of integrationg another formula app-
liese As an examplet the motion# by inertiat of a diec along a rougi
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Extremum property of'... D274/D302
horizontal surface is considered. There are 5 references: 3 Soviet-
bloc and 2 non-boviet-bloc. (both in translation), A,
Card 4A

NOVOSFJ" v S.
Extromm of the Hamiltoo.-Ostrogradskii principle in the non-
holmmic mechanics- (with summary In Suglim4l. Vest* WU no,
33:121-130 161-0 (KM 14:1)
(Mechanics, Analytic)
N

- AOVOSF.LOV , V.S.
Extrmm properties of the Ealer-laaange principle in non-
holonam,do mechanics. Veat*LGU 16 no.19:13&-I" 261. (MM 14:10)
(*chanIcs, Analytic)

33536
S/043/62/000/001/006/009
Wqqoo 111.4too D299/D303
AUTHOR: Novoselovp V.S.
TITLE: ExtremiAm property of integral principles of non-
holonomic mechanics in nonholonomiv coordinates
PERIODICAL: Leningrad. Universitet. Vestnik. Seriya matematiki,
mekhaniki i astronomiiv no. 1p 19 19620 124 - 133
TEXT: Variational apparatus (up to the second order) in nonlinear,
nonholonomic coordinates is developed; formulas are derived for the
second variations of the integrals of the Hamilton-Ostrogradskiy
and Euler-Lagrange principles in same coordinates. For nonholonomic
systems with constraints of the Chetayev type and variations as
defined by Voronets, the Hamilton-Ostrogradakiy principle is writ-
ten in nonholonomic coordinates as follows:
t2 1j
Ldt = Op 19 2p t 1; 1
~1 levitl = Slevlt2 = 0 (1.2)
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Extremum property of integral ... D299/D303
The kinematic characteristics e., corresponding to the nonholonomic
coordinates Yiq are introduced by formulas
eV = eV (qiq 4iP OF (1-3)
1+k = Fk (qiO 40 t)'
The variations (as defined by Voronets) in nonholonomic coordina-
tes are
Se d Ir,
,
8
w'6V 6.,JY 0.
Z J J +k
j=1
(1-5)
The functional
,J t2 'j
V Ldt
(in nonholonomic coordinates) has a minimum on the real trajectory
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8/04 6416061009'
0/0
-integral
ExtremUm property! of D299M3023
his
-or amia'I of 'integration ' As nonholonomic coordihat"lo
jnore gentral.'thin lagrangLan coordinatesq- it is of interest Ide-
velop~~.,formal~-*ari:atio~nEi1 apparatus in such coordinates, and 'to di-
~ y, cale'ulate on that bats. A direcit expression is derived
rectl
__Ifor t.he-.Etoooiici-,Vii~i6Ltidzl.'of:~hLi Hamilton-Ostrogradakiy functional
in 'nnnhol'onomi-d coordinates.. -After computationst one obtains
84 82 84
i, L
(2.6)
~Vy
Y
63id 'A bjqt + 0(t2 ~0*1.
where bvv ---i:a8vp cc being ah'infihitesimal quantity* If the equa-
tions-for the Ohetayev-constraints are homogeneous in 4ip-the Buler
-Lagrange principle can be written-in nonholonomic coordinates
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..Extreffnim property of integral D299/D303
-77-777:777
-A 2T
'Art (L
a
(3-3)
i awto ~=O~
The following.theorem is -p rovedtIn determining the Voronets-varia-
tion for mechanical systems with stationary.homogeneous Chetayev-
constraiAts of first order, -the --Xuler-X~agrange functional in nonho-
coordinates (of first order) has a minimum on
the real trajectory for small domains of integratione The above re-
sults are illustrated by an.example of S.A.- Chaplygin (Ref. 6: Iss-
ledovaniya po dinamike negolohomnykh eistem (Investigating the Dj-
namics of Nonholonomic Systems)# M.-Lo GITT'J, 1'149); this example
involves rotation of a solid body about its ve ical axis. There
are 6 references: 5 Soviet-bloc and 1 non-Boviet-bloev (in transla-
tion).
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.MTHOR:
TITLE:
PERIODICAL:
S/146/62/005/003/014/OL4
D234/D303
NovoselovV V.S.
Shock tests of measuring instruments
Izvestiya vysshikh uchebnykh zavedeniy. Priboro-
st-:-oyaniye, V. 51 no. 31, 1962, 141-149
TMCT: TIm author describes a part of the results.of an in-
vestigation on the design of shock absorbers conducted at the labora-
tory of vibrations of LGU. Conditions of the shock tests, experi-
Mental- study of these on a plate and transition shields (iAre tenso-
meters, high-speed filmingr and oscillograms we;re'appliegl) are des-
cribed. Dynamical characteristics of the shocks obtained by study-
ing the oscillograms are discussed. rzcperimental investigation of
shock conditions of instruments provided with a shock absorber is
described and illustrated vith examples. 'Mere are 7 figures.,
ASSOCIATION: - Leningradskiy ordena, Lenina gosudarstvemyy universi&-
tet iri.* A.A. Z*adanova (Leningrad State University im".
Card ~/2 A.A. Zhdanov)

S/146
./62/00-5/003/014/014
Shocic tests ol! measuring instruments D234/DS08
SUM-11TTED: November 10, 1961
Card 2/2

NOVOSELOVO V.S.
Structural dwacteristles of rubber shook absorbers. lxv.rfs.-
uchob.uv.; prib. 5 no-41105-114 162. OURA 150)
1. Laningradakiy ordena Lenim gosudarstvannyy universitat
Imeni A.A.Zhdanova. Rakomendovana. kafedroy tooratichaskoy
makhaniki. -
- (Shook absorbers)

- NOVOSELOV,
Extremum properties of the integral principles of nonholonomic
mechanics in nonbolonomic coordinates. West. LGU 17 no.1:124-133
962. (KIRA 1 ':,. 1)
(Mechanics, Analytic)

Ns~i or a rubber-cushlonod Instrument mchanim durIM
Impact tests. Isv. vp. ucheb. Saw.1 Wdb. 6 mo.ZQ07-224
163. OM 16:4)
L lieningradqkLy ordena lAnina gogmda"tyemWy vnivereltat
Imeld A. A. ;hdanova, Rekomendavans. kafedroy teorstichaskoy
makkaniki.
(Shook absorbers)
Nbasuring instrwments-Testing)

MOVOSE-LOVO V.S.
Optlzme double-izpalse transfer betimen orbits with ffmn
I&I.Inations mid eccentricities,, Biul,lnst.toorastron. 9
1~6-52295-309 !63. 174)

-4V.,YjU 'oLYA.F1
F -IOV, N.N. , otv, reel.;
""p-NOVOrAW
MATVFYEVA,
(Djnamica of a material polnt; mathodologIcal instnictions
no.3, on the course of theoretical mechanics for the third-
year correspondence obidents In state universities with
specialties "Ma them, ati,-~s , 11 "Mechanics" and "Astronon7"] Di.-
namika materiallnoi to~~hkl; rietodichoskie ukazaniia No.3.
po kursu teoreticheskoi makhaniki diia studentov III kursa
zaochnogo o1racherdia goaudnrstvezinykh undversitnt,ov po
spetsiallnos-tiam 4NaLe7vq.tika,~' 'T~,Ahenikall j "Astronamila."
Leningrad$ 1964. 33 p. (xim a-!.-9)
1, Leningrad, Universite-t. (Adel zao,-?hnogo obichenJya. Ma-
tematikc-mekhanicheskiy fakul7tet.

NOVOSM'107~ Yc:.
Icjr. 31
2-3 11 :64 19:2)
1.
ncg a i 'Aomi;-~= a r,,qg a in~~ -~i.a li.ns L rc;yu-.: yi T ",,So

8/0179164/0001001/0101/0103,
ACCUSION 016. AP40.18429
~AutAORt violoolov V. 'So (Leningrad)'
:1TITLE-1 Influence of it transient lcombus.tLou regime and rotation
10 -as the stain vector and mat mouent of the reaction fcccf
he n
.-t rocke-t
-4#$No taw@ Vtd, tekhi asuki Makhaniks m a *at %
-_,.$oVjtC91t AN I ashiso troy y
ITOM TAM rocket propulsion# rocket, Coriolis force, combustion
ABSTRACT t When the combustLon,chamber is rotating rapidly with the I
ensine.operating, the Coriolts'forces and moments may reach v ry
high Valu*$* Several evolved equations show that this depend: on
~the`,4ngu Lac velocity of rat tlon* The Coriolis forces and moments
a
must be considered to the favesittitation of long duration rocket flijost
especially when investigating stability., The Coriolis forces and
1-momeniog as well.as the relative acceleration of particles, aLsai-
ificantly,'Influenee the~matlon of rackets of the I* Ve Hashchorskiy
typ Ia kat length and-tho:rolative velocity of
where L-Le.the roe
particle disebarse urcreated.by pump As cesipacati,vely low* For
1/2

flit "-N, -;f/pi~ 4
AC&tIBI~*,0# --NX-v AP404446-3
43/f
AUTHORs to~i~6601ov v S
Ain
TITLZ I Application of analytic d mice methods in the theory of
optimal flights
SOURCE: Leningrad. Univc:sitet. Vestnik. Seriya matematiki,
i Mekhaniki i astronomiip not 3, 1964, 133-146
TOPIC TAGSt analytic dynamics, optimum proc-ess# optimal fligh t
opcimal trsnofer, Pontryagin principle, Weierstrass condition,
performance functioual
-",13 T-R M; T t- The methods of analytic mechanics are applied to the
u-d f
s
t-7 0 1 _ego
a a lsuimp.k-i oils, a- t' them -behavior of the control plant is deser.ibed
by and that the control,-
b-~ o
optimal control is defined an the selection from the got of allow"
Card 1/3

ACCESSION SRI AP4044463
&blv control functions of a control function such that the sy 5 tem
6--takaa from~thx inittal atate to the terminal state in a finite
vwl toollky d
ditional thd-firot variation of the porform4nce functional Li
The oxprespiou derivad is integrated Dver the specially defined
-yti
-anal -a-me Manizq,q_T
d&f VdVidw-ot' it ohe,- 'ov t m n ma.
e --irkiace:saary con
performance functional consists in determining the maximum of the
Hamiltonian function on the apti-nal tr'ilectory. Thts condition coin-
cides with the principal cond"Ition of the maximum principle of
Pontryd8in and is equivalent ro the 4ciertrass optimality condition&
Additional conditions are presented under whic"'i the necessary opti-
Malfty condition will be also The possibility of deter-
mining the optimum control !Aii! 1to-n-,73robi method is indi-
di,"
no a
ferential equation. As an example of the application of the Hatwil-
tan--.Jacobi method, the optimaL impulse transfere between two allip-
Ca r-c-2 / 3

C)
ACCESST09 NRI AP4044463
tic coplanar orbits in the gravitational,field of a symmetric central
body are considered. Equations describing optimal impulse transferee,
58 f-ormulas,
are derived, Origa A-4t; hast
-Htss T-31 0
1, 5 UB14IT-TE W NEI -14 XIj L 0
SUB CODE MA NO Ittr SOV: 006 OTHERt' 003
-771
113

NOVOSFJDV, V.S.
Use of-t~e methods of analytic dynazics In the theory of
optlaum filghts. 7est. WU 19 no.13t133-146 t64,(HTRA 1728)

NO - I ~-",
C-Dtir-nbq space ascent. of ar interapianetary rocket to a
orbit, Uch- Zap, LGU no,323.169-182 164,
( 'Cl RA In/ ; 12 )

NOVOSELOV, Viktor Sergeyevich; POLYAMOV, N.N., otv. red. I
(Dinamics of a material system; methodological instructions
No.1 on the course of theoretical mechanics for third year
correspondence students of state universities specializing
in "Mathematics," "Mechanics" and "AstrananTfll Dinamika ma-
terialInc' sistemy; metodichaskie ukazaniia No.1 po karsu
teoretichaskoi makhaniki dlia studentov III kursa, zaocbnogo
obuoheni-a gosudarstyanafth universitatov po spetsip"no-
stiam "Matematika," 'Hokhanika," i "Astronomiia.0 Leningrad,
1964. 40 P. (MIRA 18:3)
1, Leningrad, Universitet, Otdol saochnogo obuchenlya.
Matematiko-makhanicheakiy fakulstato

NCIVOSMUR V.S.
. -1.1 M- -1%--1-.t----., I ---l-,
DEngireering, calculation of optimum shr,-,k. absorptJon of
menhhniums in shock-resistant instruments. lIzv.vys.uckeb.zav.;
F---Ibo 7 no.6s98-104 164. (,MT RA 18:2)
1. lkningradskiy ordena Lanina gosudarstvennyy unIv-arsitet iment
Didanova. Rekamendovana kafedroy teoreticbeakoy mekhatil ki .

c )AP: :A F r-), 17, a ej -
-~N N'R: iVI ',-~ C, 12 3 3 P,
-.0 4
X!go%lov, V. S.
Change in the radius of a
:,r.,i - ix, e P~han e
F: LeiniLzraq . lip, -Ive rs i tt,.
9r
AGS combustion, irr~,p], e r:i ~i., --,i7 1-:q,id
eritnous commbust
`TTA,- T: "Ine motion of' a droplet of fuel -ela-ve tQ 5. '-ori zontal s'~-.ream of aJr
4 th- rhanges of its radius due to evaporation were analLyzed, A f Ormula describing
aT i,&z-. of tine dr:~p_'et ~k s .1 W~ f r
a for-mu-'a ~xpre~ r: 7~cnt~iI c"ue o -.~va--
Grig, ext. bas o 17.z AC'
nore
Sj i7B --3
02r),t64 N E: PR
F SOV: ESS: 4001)
DO 3 A- R

MONSELOV VIS,
Possibly simat transfer in the field of central force. 11ch.zapACU
so*3289150-159 165, (KIRA M10)

NOVOSEIA)V, V4S.
Theory of the approximate solution of variatJonal problens and its
application to the study of the motion of a point of variable mass.
Vest. LGU 20 no.1:110-120 165. (MIRA 18-2)

NOVOSELE~z ~V.S.
Variation of the radius of a spherical droplet. Vest LGU
20 no.7:163-164 165. (KMA 18:5)

NOVOSELOV, V.S.
Trajector7 of a point of variable mass in the central fields Vest.
IGU 20 no*19:347-156 165, (MIRA 18110)

L 05
861-67 EXP(c-)/'K4T(1) TJP(c) qD
Acc NKs ATW224T4 (A) SOURCE CODE:::U.B/0000165/000/000/0liFl/0152
AUMMR: V. S.
None
ell
TITLE: Analytical dynamics and optimum flight paths
SOURCE: Vaesoyuznyy s"yezd po teoreticheskoy i prikladnoy mekhanike. 2d, Moscow, 1964,
Analitichaskaya mekhanika. Ustoychivost' dvizheniya. Nebesnaya ballistika, (Analytical
mIechanics. Stabillty of motion. Celestial baUistice); trudy s"yezda, no. 1. KbaccV,
izd-vo Nauka, 1965, 141-152
TOPIC TAGS: Hamiltonian Jacobi equation, optimum trajectory, motion mechanics
ABSTRACT: The author considers an object vith an equation motion- having the form
where uk(t) are controls or controlling functions which may be-piecevise-cal2tinuous,
and t is time. The controls should satisfy the conditions
Uft UA, < UAS, U&I CM-St, U&I =const.

ACC NRI AT6022474 0
In particular the conditions a" co, uks =_ oo may be fulfil-led for all 'or some con
trols. It is assumed that a unique trajectory in the given system corresponds to any.
permissible control and the explicit conditions relating the-boundary values of the *
variables in the general case are given in terms of the coordinates of the initial and
final points of the trajectory with respect to time. Controls are chosen to give a
minimirm value to a given functional calculated on these controls. The Hanilton-
Jacobi method is used for solving the system of canon'ical equations which determine
the optimun.trajectory of the given object. Orig. art. has: 41 formulas.
SUB CODE: 12/ SUBM DATE: 04Dec65/ ORIG IW: 008/ OM PJW: 006
kh
V E/2

rap
Novoselov. Vikto r Sergeyevich
Variation methods In mechanics (Variatsionnyye
[Lenhwad1'Tzd-vo Leningrad. unly., 1966. 66
printed*
metody Y zekhanIke)
p. biblio. 5900 copies
TOPIC TAGS: analytic sechanics, variational nothodjintegral principle
PURPOSE AND COVERAGE: This book contains a brief elucidation, usually
without proofs of the theorems and final fq
,Vmulasg of the basic
concepts and methods of analytic mechanicsM It discusses some
methods for applying the calculus of variations to analytic
mechanics and the properties of the trajectories of mechanical
systems with holonomic and nonholonomic constraints of the Appel-
Chetayev type. The stationarity and the minimality of the Hamilton-
Ostrogradokiy and the Ruler-Lagrange integral principles are dis-
cussed; the minimality of the Gauss principle Is justified for
mechanical systems of this type; and the integral Invariants of
canonical systems, contact transformations, the Hamilton-Jacobi
method of integration, and perturbation theory are discussed* The
book is intended for scientists, engineers, graduate students, and
advanced undergraduates as a brief but comparatively complete guide
to modern methods of analytic mechanics.
Card I / 2

L 05071-67
ACC NR-. Am6olaM
TABLE OFCONTENTS (abridged):
Foreword -- 3
Introduction
Ch. 1. DIAlembert-Lagrange variation of holonomic systems -- 5
Ch. 11. D I Alembert-L!LjiEjLpjtS_yj~.F1&t Lon or nonholonomic system* 21
Ch, III. Gaussian variation
Ch. IV. A theory of optimal processes based on the methods of
au&lytLe mechanics -- 58
Basic notation .- 68
Index -- 69
Bibliography -- TO
SUB CODZt 20/ SUBM DAM OTF*b66/ ORIG REP: 026,

MWI*M"v reo (Kazan$)
I -
Fundamentals of classical-analysis and the theory of analytic
functions in a -poljndic region* Izv. vys. ucheb., sav.; mat, no,
5s-71-88 163. (MM 16:
n)

GALAM, G.I.OT9S~kqv,,Te,N.
Baikal. Irkutsk,, Limnologicheakii in-t Sibirskogo otd-
niia AN SSSR. 1964. 1 v. (MIRA 18:3)

KOVOSUM To S. Inshenero
WAR-1 1-00
Dmm3Lopmnt of On building and road constr=tIon mah1nez7
Industr7. YAO&.strol.12 no.1:3-10 4T&155* (mm 8:3)
1. Ministr strottelinogo 1 dorozhmgo mashinostroyonlyso
(Building mwhinery) (Road wchInGz7)

NOVOMOV U.S.
lomoidlate task@ of the ball4ing oind rc&4 machlner7 Inolustry.5trol.
I dor.mehinostv. 1 A 156. (KERA 10:1)
1. Klnlstr strolt*llnogo I doro-shnogo mshtnostroVenlya.
(Building machinery industry) (Road mchtnery)

NDTOSEMV. Y6 S
Building and road construction machinery manufacture In thw
sixth five-yoar plan. Kakh. trud. rab. 10 no.8:28-31 Ag 156,
UM 9:10)
1. Kinistr strottellnogo I doroshnogo mashinostroyanlya.
(Building machinery) (Road machinery)

lovom", ro.s.
.-, ~ , - --;
Bulldlm aM road machinery Industry lu the sixth five-year plan.
Ylmkh.s~rol.13 no.11:5-11 1 156. (WAVA 9:12)
l.Slulatr strattellpago I doroshnogo mahimantroyenlya.
(Road machinery) (Building uschinery Industry)

NDVDSEI_0V' C.
AIJTHOR-.
None - given. 5
-_-TITZI: Problems of Pleahanization Discussed at an All-Soviet
Conference on Building,,. (Voprosy mekhanizatsii na
vsesoyu--nom sevesA. 4
hchan-Li pc stroitel'stva).
PI$RIODICAL: Mekhanizatsiya Stz~oitell stva, 1958 Jq Nr 5, pp 3-7.
ABSTRACT: An All-Mdon Conference on 'building organized by
the TsK KPSS and the Council of Ministers of VA* MSR
was held in Moscow -tetween 10th and l2th April 1958.
'hu ' zat ion
The main topics disaassed were buildil2a, med . d
and the manufact,,ire of building, and road buiiding
machines. (Main speakers:Ye. S.Novoselov, Minister
and Head of the rrcsplan of-U-MT-a-07 =.. Levin.. Chair-
man of the Gosstroy of USSR4 Mr. Novoselov read a
paper on the mecheirLzation and the manufacture of
building and road building machines during the period
.1955/51. Engineer N. Y&.Ko=1o-d of Glavmosstroy pre-
sented a ,new implement for the manufacture of fencing
and external walls. Mr. Levin of Gosstroy of USSR
reported on the. 'Morease in the number of building
machines since the second A.11-Soviet Conference on
building. At present tb-e Gosstroy of USSR has 19
Card 1/2

sovAOO-58-5-1/15
Problems of Mechani zati o-.: DJ sri~zssed at an A-I-Soviet, Conference
on aa
factories for the mai-tenanca of building machines.
The manufacture of with a capacity of 75 tons
is advccated due to the increasing use of precast
reinfc,rced concrete uc--.~stxuct ions. Ur. i'lo-stotiskiy
of Gcsplan -;f uSSIR requested the manufaQture of
certain types of small machines and instruments re-
quired in the buildingtrade.-i. Odiotm6tion workefd
,Tishchenko, Gnltla-av and Kuzneisov pointed out tlie
shortcomings of exc;w;&,.tor:;3 mamufa2tured by I'Ralbochiy
hetallist." factory. The sera,~er D-374 was reconstructed.
Engineer Gor buno-k~ c�' Gi avat ro-.ymekhani zat sly* of the
ministry of Tran6portation demanded the -expansion and
co-ordination of acieYr4-ific research in the field of
maintenance of building m&:;hinery. The co-ordinating
body should be (RfIOKIIP. Akademii stroitel'st.va i
arkhitekil-'Ury SS.SR) 'KI-MVP cf the Academy of Building
and of tiSSR.
1. Construction--Equipa-att 2. Road building equipmenr--Production
Card 2/2

NoVOSELO~~
SO-11/122-58-6-32/37
AUTHOR: Korolev, A.A., Candidate of Technical Sc-ie=.es
TITIR: Dev I Prospects for the Manufacture of Metallurgical
f8puniffil" h razvitiya metallurgicheskogo mashino-
stroyeniya)
PERIODICAL: Vestnik Mashinostroyeniya, 1958, Nr 6, pp 80-82 (USSR)
ABSTRACT: A branch conference on metallurgical engineering plant,
convened at the Uralmashzavod in Sverdlovsk by the Otdel
mashinostroyeniya Gosplana (Mechanical Engineering Division
of the State Planning Commission of the USSR) is reported.
400 delegates representing 22 economic councils, 14 research
institutes 24- design institutes and 29 metallurgical
equipment manut-acturing plants were present (including the
Uralmashzavod, the Novo-Kramatorskiy zavod (Novo-Kramatorskiy
Works), Staro-Kramatorskiy mashinostroitellniy-zavod
(Staro-Kramatorsldy Plant), Zlektrostall skiy zavod tyazhelogo
mashinostroyeniya (Blektrostall Plant) ' the Yuzhno-Ural'-
skiy zavod tyazhelogo mashinostroyeni?a,(Yuzhno-Ural.'skiy
Plant), the Irkutskiy mashinostroitel nyy zavod (Irkutsk
Plant), the Novosibirskiy mashi-nostroite.Lniy zavod
(Novosibirsk Plant)) as well as 16 steel Works (including
Card 1A9 the Kagnitogorskiy metallurgicheskiy kombinat, the Azovstall,
2-

SOV/122-58-6-32/37
Developt'.qent" Prospects for the Manufacture of Pletallurgleal Equipment
the Zaporozhstall, the Novo-Tagilbkiy Works, Euznetskiy
metal lurgicheskiy kombinat (Kuznetsk YletallurCical 'oi:.-bil'o).
In his opening address, Ye-S. Novoselov, Minister oi the
USSR, emphasised that t1ii'State Pla-nni"Rng Commission attached
great importance to the conference. Vinogradov, K.K.,
deputy director of the mechanical-engineering division of
the State Planning Commission, pointed out that the
production of metallurgical equipment increased 16-fold
in theperiod between 1932 and 1957. The manufacture of
rolling-mill equipment increased 24-fold. Betmieen l9cl and
195?, 2? blast furnaces, 5? open-hearth furnaces, 35 rolling
and tube.mills were built and erected and 22 rolling mills
were completed, awaiting erection. This equipment was
responsible for an increase of 18.2 million tons of pig iron,
24.9 million tons of steel and 19-3 million tons of rolled
products. An improvement in quality and a rise in
productivity have taken place. During the period between
1959 and 1965, the manufacturers have the ta9k of con-
structing powerful blast furnaces of 1 719 m2 and even
3
2 286 m, capacity, the largest in the world. New designs
card2/9 of automatic skip hoists,, weighing carriages, charging

NUICCELOV ye.s.
lanufacture of construction machinery is the principal +-chri.-
cal basis of the consti"action industry. Stroi. i dor. mash. 9
no.1:1-3 Ja 164. (MLU 18:7)
1. Predvedatoll Gosudarst-vannogo komiteta stroitellnogo,
dorozlinogo i kommunallnogo Bins hi nos llroyenlp pri Gosstroya SSSR.

F-O'IOSEMV, Ye.s.
We welcome partiolWts to the Ekhibition. Stroj.ji dor. mash.
9 no.8:1-2 Ag 164 .. WIRA 18al)
1. Kinl- I - SSSIII i ftedsedaiiil Organ izats ionnogo kondtata f,',szbdu-
narodncrvystavki s trod tel tiiy.&h I dorozhnykh mashin i razliclu"Y'kh
sredstv-,mekhanizatsii strolteltno-montazlmykh rabot.

r'?
myos=.. TAT--
. IITooiagiciathowy of the dLviAlblUty of lhtepriv* lkh. up. ZGPI
60-23 160 (MIU 15:7)./
(Topoloa) (Ikubereq Theory of)

MOVOSELOV, IG.V.
Topological theory of polystdic numbers, Trudy Kit, Last, AN
Gruzo SSR 2761-69 160. (WRA 15:3)
(Algebraic topology)

-KOVOSEIDVI YeAl
Integmticn on one bicompact rings, and applications to the
theory.of n=bera. Izv. vya. ucheb. zav.; mat.. no.3,066-79
161. (MIU 1-4:7)
lo Ka--anakly gosudarstvennyy univeraitet imeni V*I.Mlyanova-
Janina,
(Rirgis (Algebra) )
(U=bers,, Theou of )

NOVOSEMV, Y~,.V. -
Topological and metric properties of the multiplicative
structure of prime numbers. DokI. AN SSSR W no.6.-1255-
1257 F 962. - (14M 15:2)
1. 1. Kazanskiy gosudarstvevny7 universitet Jm. III.V.Lomonosova.
Predstavleno, akademikom I.M.Vinogradovym.
(K=bers., Prime)
(Distance geometry)

ROVOSELOV, Te.v.
Sow formulae related to a reduced residue system. Dokl. AN SSSR
143 no.6:LI74-1277 Ap 162. MRA 15.4)
1. Kannskly gosudarst"nnyy universitst Im. M.Ullyanova-lanina.
Predstavleno akademikom I.M.Vinogradovym.
(Numbers, Theory of) (Congruences and residues)

PILINSKIYO V.I-., inzh.; ](OVOSEWV, .-Yu.A.,,, ~nzh.
DaterjAnItt, the'ithermal Iffeld at -tm&. Uple-pass grinding of, hard
alloys., 743t,amaaaoptz~.' 43 no.1l.-46-51 N 163. ()dOA 17.- 2)

KVALIVASSERP V.I*v kand. tekhn. nf~uk; ANDA-41,J.SHI,,VIVJI, Yu.M., kand. teb--hn. nauk,
dotsent; NOVOSELOV, Yu"., Inzh.
Effect of torsional vibrations of the d:,i,;e from the spindle to support
in the 1811 semiautomatic relieving lathe on the quality of machined
parts* Izv*vys*ucheb.zav.; mashinostr. 110.4:160m167 164, 18-1.)
1. Kuybyshevskiy politekhnicheskiy institut.

REZNTKOV, A.N.-, NOV05FLOV, Yu.A.
0
~ -'; - ~'
Approximate method for calculating temperature fields in
vedgea. Inzh. fiz. zhur, 7 no.61114-119 164* (MIRA M12)
1. Otraslawaya nauchno-proinedstvannaya instrumentalInaya,
laboratoriya,, Kuybyshev.

MOVOSELOV, Yu.A.
Old erosional surface in the Kichiga River basin* Vop. 0 .
Kamch. no. 2:106-108 164 (Mm Iral

NOVOSUGf, Yu. K.
"Effect of Grass Mixture Covers of Different Composition and Some
Other Agrotechnical Methods on the Flax Yield." Cand Agr Sci, Moscow
Agricultural Acad imeni Timryazev,, Moscow., 1953. (RZhBiol, No 4, Oct 5U)
Survey of Scientific and Technical Dissertations Defended at USSR
Higher Sducational Institutions (10)
So: Sum. No. 481, 5 May 55

Country : USSR 14
Category: Cultivated Plants. Cormnrclal. Oil-DearinG.
Sua2r-Dearine.
Abs JOUr: r=iol., No 111., 1958, No 49022
Author Noyceeloy Yu. X.
Inst Tirdryuzcv izriculturai tcud.
Title The Influence of the Standard (~=tity cuid the Manner
of SowinG oil the C~Iuality of P.Lber-Fl= Seed.
Orig Pub: rzv- Tiraryazovsk. a.-kh. akad., 1956, uo , 63-68
I'l.batz-act: In the years of 1553 and 1954, _Jnvcstige"-_'oas On
the effect of ;ho rm=er of sowing (wide.. double
and dense rous) of fiber-flax, together with dif-
ferent standard quantities, on the harvest and
qualitY of seeds have been carried out at the flax
Card 1/3
m-lo6

Country : USSR M
Category'. Cultivated Plants. Comarcial. Oil-Bearing.
SU(Ar-DearinG.
,L's Jc'L'~c: RW-401-, TO -11, 1958., No 49o22
experimental station Of the Timiryazav Arricultural
Academy. _12 the flax was planted sparsely, the
MMIber of fniits on the plants increased. The total
harvest Of smds was PractiCaUY the sam for thin
and dense sav~.n&,-, but the propagation coefficient
Ll
was higher by a factor of 2 - 5 for t' in sowing.
The format�on of scads is wre Intense in the case
of dense s(Aiin&- If the stems are thick, the abso-
lute veialit of seeds is lower. The absolute weight
of the seeds is higher in the first periods after
aced formation than at later tives. This distinction
is particularf-ly acute in the case of thin sowing.
Card 2/3

Country : USSR it
Cautcaory: Cultivated Plants Comiercial. Oil-Dearina.
Sugar-DearinC;.
Abs Jour: R=iol., No 11, 1958., Ito 49022
The mat even seed material has been obta:Lned. from
dense cultures. Vie sowing of linsceds obtained fran
sp=sely sown cultures somewhat decreases the harvest
of oeeds and quality of the straw. -- D.D. Dakhmistrov
Card 3/3
M-107

IMVDSELOV# Xu.K.p kand.sel'skQkh*xyaystve-nnykh nauk
For more -Utensive utilization of cropland in the non-Chemozm
zone. "Zenledelie 23 no.3:1&-21 Kr 961. (MMA 14:31)
10 Veen .nauchno-isoledmteltskiy inatitut kormov
Imeni.
(Agriculture)

NGVOSMV, Yu.K.,q kand..sellkhoz. nauk; RO,GGV.. M.S.; POLYAKOVA., V,,, red.;
7 TUMZEBK3NAq M.p tekbn. red*
[Raising forage beans for seed) Kormovye boby na semen&. Koskva,
Mosk, rabochii, 1962, 24 p, (=A 1516)
1. NaucbzWy rabotnik volostnogo lspolnitellnop
komlteta Moqkcvskoy oblasti (for Rogov).
(Moscow Province-Beam)

#:I.De, kand.mel'okokhoz.rauk; K=VWSM, kand.sellskokhox.
okh
UVA- j-Tu.K., kand.sellsk os.nw*
NImd pbmtIvgo and the Swedish fly# Uohchraxt,ot vrtdi bol,
7 no.037-38 Ap 162. (MM 1502)
lo Toeoo7u=37 institut cashchit7 ranteuiy (for Sha iro). 2., Vseso-
yu=W institat kormov (for Karavymnokiy, govooelcW5
~(Gorn (Wive))-Diseases and pests) (Trit flies)

KOREIMSKIYP B.S.; 11
Standardizing electric actuating mechanisms. Standartizatsila 25
no46:22-24 A 161.' (MM 14:6)
I (Electric motora-Standards)
i

137-58-4-8434
Translation from; Referativnyy zhurnal, Metallurgiya, 1958, Nr 4, p 302 (USSR)
AUTHOR: N ke
TITLE: Rare Elements (Redkiye elementy)
PERIODIC-AL. Oktyabr', 1957.. Nr 9, pp 177-179
ABSTRACT: Bibliographic entry
!. Rare earth elements-Bibliography
Card 1/1

MMLINA, IT.G.; MUO4N1QT 0__A! - RYCHKOV, R.S.
Dissolution of micropowders of fused aluminum oxide and the
determination of impurities It contains. Zav.lab. no.11:1293-1294
159. (MIRA 13:4)
(Aluminum oxides) (Metala-- Analysis)

3/020J62/147/004/018/027
RIOT/Ble6
.,'AUTHORS.- _1orenev#-.,. M.' Simanov,, Yu. Pf"~ (Deceased),
an YU
'16yosel 'A~ A
I Corresponding Member AS-USSR
ova,
-TITLE: Vihombic-mod'ification of ber~yllium -fluoride
JPERIODICAL: Akademiya nauk SSSRi Dokladjy,v;~-147, no. 4, 1962, 846-848
I structures. So
-TEXT i - e struct,urps Be? are similar to-thi 5 P2
th
2
;ypei 0'.-structures have been found, -oquartz# a-quartz,
far, the foll6wIngA
till.4 - i "-' " d r
cristabali e,:an _a-c ~is obalitO. i The present, paper describes a news
ifioibiic mod if ic' t ion f B' F. w1i Itch'' is ' s -to ~"be -' f structure similar
-A a 0 a a Butwed, 0
to, tridymi .te. -1his mod if id4tion
had already been detected, during the
thermal Big Of ~the NaF -BeF eystenjA.Y.."Novoseloya, M.Ye. Levinal
at-
and M. P i 'Save 11 ieva'.. zhxKht v. ~ 3,1: 2 562 (1956)
4." ~), Ut, It could not be found'
succel
0-0 b 'photography'.;, Thel.authore-* tdad in piftparing a mixture of
Z y X-4ay 0
gefZ_ contain ij '-'4%`ZrF an n
ig 00, 0 d 20 ma Ng argo pressure
tat ~590'
der Ratterne were
by..25a'-hr temp ring.suitablej, or.X-ray 6ha Y8 S.,
01Q-rd V
'Card 1/3

.810
rhombi* modification of 2YO62/147/004/018/027
B10
B
7, B186
~,---ASSOCIATION: Moskjvskiy gosudarstvennyy universitet Im. M.V. Lomonosova
(Ito ow.Stat Universit imeni X.V, Lomon-
y 0807)
SUBMITTED: July 18, 1962

LEYKDi. Ye.R.; GUTIRA, SjL.; CMMMM, I.K.; GRANKINA, L.d.;
PAVW, A.A.; NWOMWVA, A.A.
Introducing tIm-tattery method ror ion-exchangs p~rirlcatlon
or xylose syra". Gidro3-ts* i lemokhim. prom. 16 no.2:35-16
'63. UMA 16t. 6)
1. GosudarstvmmW nauchno-issladovatellskly institut g1dro-
Usnay i aullfitnospirtovoy prmyshlennosti (for Leykin,
Gutina). 2. FerganskLy -gidrolizrWy savod (for Cherazukhin,
Grankina, Favlov, Novoselova).
(171086) (ion exchange)

A-
r
US=/ Physical Choodstry - Crystals B-5
Abs Jour : Referat Zhur - KhI-Iya,, No 4, 1957P 10941
Author : Kirkins, D.P., MovogAlouLA.B..
Inst- : AimdmW of Sct;HEes EAM , . Simonov Yu.P.
Title : On Pblywrphim of Berylliun Pluoride
orig Pub : D*l. m sm, 1956., 1o7,, so 6, 837-838
Abstract : fttram=, BeF2 (1) formed an thermal decompositidn, of axw=lus fluoro-beryl-
late and having the structure of low-tempertture chrlstobalite,, In endother-
ALU,y transfornied at 130P into cubic form (face centered lattice, a 6.78,
kX)J, analogmw to the high-teMpratu" fam of christobalite. In a numflmr
Of Instances on heating of 1: endotherna effect to observed-st 40& but
trawforwtion into now form lernot revealed'rowt grOphically. I be-
gins to Mit at 5W but main bulk of I =Its at 7W; steNise wArng
of I indicates slow transfornstion of Its nodifacations.
I nist'be regarded as a pseudo single-componimt system.
Card 1/1

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KOROVINO A.L.; ROTOSSWTA. A.1. -,- XASTOROTIGH, R.A.
ClInIml ani IMor&tory chmacterlstlas of laluessal p~monla.
Trw4y AUK SSM 28;189-197 -28:199~-197 153. Off-RA 7: 8)
1, U Ot4ol& vlrusologll lostituta opidentologil Is. ftatera I
propedowtichodwy toropwtIoUskoy klinikl I Lonlogradskago
seditsinskago Umtltuta In. LP,.Pavlova.
Inf IUMS&I pasononla)
luf lusual pneumonla)

YOUSUOTA A.I..; GOMMOT. S.F., daktor meditsinskikh nauk. zavedayushchiv;
A.. professor. direktor.
ZVWhanglom of the right log. Test.,khir. 73 no.5:65-66 S-0 153.
(MLaA 6:11)
1. ILiniks protestrovanlya LentWadekogo usuchno-lesUdavatellskago Inatitata
protestrovanlya. (TqWh&t1cs-Twwrs) (Leg-%mors)

NDTOSMTA. A. 1.
Nobillsation of stumps of the upper extradtles. Test-kh" .74
zo.7:63-" G-11 154. (NLM S:ILOj
1. Is kllngd protestroyanlya (=Y.-d~r moditslook1kh nock,
S.F.CWwwv) Lonlogra"bW nouchno-losladavatoltakW institute.
'Protestrovanlya Adras avtora: Leningrad, Boroways. u1. D 78,kw. 11.
(AMMAMN S2W,
am, nabilization)

GaMOV. S.F..doktor med. nauk; NOVOSILOVA. A.1.
Levels and methods of amputation in nocrosts of the extremities
In endarteritis oblitorans. Test. khir. 76 no.11:38-45 155
(MM 9--4)
1. Is kliniki prot4wLrovanlya. (zav.--doktor moditsinskikh nauk S.F.
Godunar) Laningradukogo nauchno-issladovatellskogo instituts,
protezirawanlya.
(SiDARMMS OHLRMWS. compl. surg.,
necrosis of extremities. levels & methods of amputation)
(13MMITINS. gangrene.
caused b7 andarteritis obliterans. surg., levels &
methods of amputation)
(GAHM=.
extremities, caused by endarteritis obliterans, surg.,
levels & methods of amputation)