SCIENTIFIC ABSTRACT GALKIN, S.I. - GALKIN, V.S.

• Document Type: CREST
• Collection: Scientific Abstracts
• Document Number (FOIA) /ESDN (CREST): CIA-RDP86-00513R000614120005-2
• Release Decision: RIF
• Original Classification: S
• Document Page Count: 100
• Document Creation Date: November 2, 2016
• Document Release Date: July 19, 2001
• Sequence Number: 5
• Publication Date: December 31, 1967
• Content Type: SCIENTIFIC ABSTRACT

Problems In Calculating Aircraft (Cont.)
SOV/2606
Stability equations are obtained for a cylindrical
sandwich shell consisting of two thin outer layers and
a corrugated middle layer. The problems of stability
of a curved sandwich panel simply supported along
its four edges and of a cylinder under compression are
solved.
5.' Kurshin, L.M. Stability Under Compression of a Curved
Cylindrical Sandwich Panel the Transverse Edges of Which
Are Fastened %jiile the Longitudinal Edges Are Simply
Supported
This paper analyzes the stability of a cylindrical
sandwich panel with a light isot3~opic core under
uniform longitudinal compression for a case where
the transverse edges are fastened and the longitudinal
edges are simply supported.
6. Kurshin, L.M. On the Calculation of Bending Stiffness of
the Outer Layer of a Curved Sandwich Panel Under Longi-
tudinal Compression
Card 4/7
69
80

Problems in Calculating Aircraft (Cont.) SOV/2606
A formula is obtained for calculating curved sand-
wich panels under longitudinal compression with
consideration of the natural bending stiffness of
the outer layers. The domain is established in which
the assemption of this btiffness being equal to zero
is applicable.
7. Galkin, S.I. Torsion of an Open Cylindrical Shell Rein-
rnra-eCb~yBu.kheads 85
To-rsion of an open cylindrical shell reinforced by
bulkheads is considered in this paper. The solution
is obtained without introduction of additional hypotheses
aside from the general assumptions associated with
representing the operation of-an open shell as moment-
less. On the basis of the solution the limits of
applicability are shown of the hypothesis of warping
which has been widely used in problems of calculating
open shells under torsion.
8. Galkin, S.I. Torsion and Bending of a Circular Cylindrical
Shell. Reinforced by Elastic Bulkheads 102
Card 5/7

Problems in Calculating Aircraft (Cont.) sov/206o6
This paper Investigated the state of stress of a circular
cylindrical shell which is reinforced by elastic bulk-
heads and loaded along the edges by an arbitrary system
of axial and tangential forces. Calculation formulas
are obtained which permit calculating all elastic-defor-
mation components for various boundary conditions at
the edges of the shell. The effect of self-balancing
forces on the state of stress of the shell as a function
of the stiffness of the bulkheads was investigated. It
is shown that the self-balancing stresses do not decay
very rapidly; the zone of their propagation into the
depth of the shell is practically equal to the length of
the contour of the transverse cross section of the shell.
A calculation example is given for a shell under torsion
allowing for elaBticity of the bulkheads.
9. Nazarov, N.I., M.S. Povarnitsyn, and Ye. V. Yurlova.
Calculation of Unsteady Temperatures in an I-beam Element 142
This paper presents two methods of calculating the
temperature fields in an I-beam element (repreBenting,
in this particular case, a typical'part of a multilongeron
Card 6/7

Problems In Calculating Aircraft (Cont.) SOV/2606
wing): 1) the method of direct integration of the
heat-conduction equations, and 2) the method of
elementary equilibrium. Cases of symmetrical and.',*
unsymmetrical heating of such elements through the
outer flange surfaces are cons2gered as well as the
case of different thicknesses of flanges. Solution
of the problem is given under the assumption that
physical characteristics of the material and the
heat-transfer coefficients do not depend on temperature
variation.
AVAILABLE; Library of Congreas
IS/Mg
Card 7/7 11-24-59

SOV/147-59-2-7/20
AUTHORS: Galkin, S.I., Kabanov, V.V. and Lyashenko, S.S.(.Novosibirsk)
TITLE: Experimental Investigation of Bending of a Cantilever
(Circular) Cylindrical Shell with a Large Rectangular
Cut-Out when Loaded by a Concentrated Force at the
Free End (Eksperimei,tallnoye isaledovaniye
karkasirovannoy krugovoy tsilindricheskoy obolochki s
bol'shim pryamougolinym vyrezom pri izgibe
sosredotochennoy siloy)
PERIODICAL;Izvestiya vysshikh uchebnykh zavedeniy, Aviatsionnaya
tekhnika, 1959, Nr 2, pp 49-61 (USSR)
ABSTRACT: The experiments were carried out on a shell of
600 mm diameter, 3800 mm long, plated with D16AT
of 0.8 mm thickness. The shell was stit'.rened on the
outside by longitudinal stringers (pressed dural 2
angles, Pr 100-3, of a cross-sectional area of 0.434 cm
and on the inside by ribs spaced at 130 mm. The total
length of the cut-out was 1000 mm. The general
lay-out of the shell is shown in Fig 1, while Fig 2
shows the cross-section of the rib. Along their whole
length the longitudinal edges of the cut-out were
Card 1/5 reinforced by either channels with flat fillets or

SOV/147-59-2-7/20
Experimental Investigation of Banding of a Cantilever (Circular)
Cylindrical Shell with a Large Rectangular Cut-Out when Loaded by
a Concentrated Force at the Free End
simply by flats, as shown in Fig 3. In the plane of
symmetry of the shell (1.e. with respect to cut-out)
two longitudinal joints were made. One end of the
shell was firmly fixed (by means of a fitting attached
to a steel plate) and the shell was loaded at the
other (free) end, the force being applied with the aid
of cables to a short steel cylinder which was fitted
into the shell (see Fig 1). The force was measured by
a spring dynamometer. Two different directions of
loading were used, as shown in Fig 4. In the first
case :the force vector was in the plane of symmetry of
the structure and in the second case, in the axial
plane perpendicular to the plane of symmetry. Fig 5
shows the complete rig ready for experiments. The
results of experiments are presented in Figures 7 to
14. The graphs also include the theoretical curves
obtained from relations developed in Ref 1. All
experimental data and the computational values refer
Card 2/5 to the same loading, viz 1000 kg. Figures 7 to 10

SOV/147-59-2-7/20
Experimental Investigation of Bending of a Cantilever (Circular)
Cylindrical Shell with a Large Rectangular Cut-out when Loaded by
a Concentrated Force at the Free End
refer to the symmetric loading (case 1) and Figures
11 to 14 refer to the asymmetric loading (case 2) as
follows: Fig 7 shows the tangential stresses in the
open portion of the shell (at sections I and 4, see
Fig 1). It is seen that they do not remain constant
and are greatest between the 8th and 9th stringers.
It also appears that the strength of the longitudinal
reinforcement on the edges of the cut-out has
essentially only a local effect on the magnitude of
stresses in the panel at the boundary of the cut-out.
There is good agreement between the calculated and
the experimental results. From Fig 8, which refers
to sections 5 and 7, it is seen that in the closed
portion of the shell the distribution of tangential
stresses is extremely non-uniform, showing even local
concentration of stresses. The peaks in the stress
Card 3/5 curves become less sharp further away from the cut-out.

SOY/147-59-2-7/20
Experimental Investigation of Bending of a Cantilever (Circular)
Cylindrical Shell with a Large Rectangular Cut-Out when Loaded by
a Concentrated Force at the Pree End
The strength of the reinforcement on the edges of
the cut-out has an insignificant influence on the
distribution of the tangential stresses. Fig 9 shows
the normal stresses at sections 1, 4 and 5, while in
Fig 10 the normal stress along the stringers Nr 1 and
Nr 9 are shown, the last one being the reinforcement
of the cut-out edge. Again there is good agreement
between the experiment and the theory of Ref 1.
For the case of the asymmetric loading the conclusions
may be summarised as follows% The distribution of
tangential stresses in the open part of the shell
(Fig 11 refers to sections 1 and 4) again is not
constant. The strength of the reinforcement on the
cut-out edge again has only a local effecti influencing
the stresses in the panel between the 8th and 9th stringes.
Agreement between the experiment and the theory of
Ref 1 is much poorer than in the previous case. In the
closed part of the shell the distribution of tangential
Card 4/5 stresses is also non-uniform (Fig 12, sections 5 and 7)o

SOV/147-59-2-7/20
Experimental investigation of Bending of a Cantilever (Circular)
Cylindrical Shell with a Large Rectangular Cut-Out when Loaded by
a Concentrated Force at the Free End
The non-uni ormi-ty becomes. lezs. i_utensie further away
from the cut-out into the clos:dtpart of the shell.
The strength of the reinforcem n has fundamentally a
local effect influencing only the maximum stress
arising in the panel between the 9th and 10th stringers.
Agreement between the calculated normal stresses and
the experimental values (Fig 13) is good at Section 1
(at the middle of the cut-out) but poor at the
boundary of the cut-out (section 4). Fig 14 represents
the distribution of normal stresses in the stringers
Nr 9 and Nv 5. Theve ax-e 14 rigures and I soviet
reference.
SUBMITTED: October 21, 1958
Card 5/5

S/124/62/000/010/013 5"----
/O1
D234/D308
AUTHOR. Galkin, S. 1.
TITLE: Torsion of an open cylindrical shell reinforced by
fra me s'
.PERIODICAL: .Referativnyy zhurnall Mekhanika, no. 10, 19629 9, ab-
stract 10V59 (Inveollection: Vopr. rascheta*elementov
aviats. konstruktsiy', no.-1, M., Oborongiz, 1959,
85-101)
TEXT: The author considers the solution,of the problem of stressed
and deformed state of an..open momentless cylindrical shell subjec'
to torques applied along-the ends. The longitudinal edges are re-
inforced by beams, the shell consists of several sections reinfor-
ced by frames at their joints.' The author uses difference-differ-
.ential equations obtained by L. I. Balabukh and integral boundary
conditions. A complete solution is given for ~;shell consisting
of two-sections. The solution is illustrated by" graphs of distribu-
-tion of forces along theJength of the shell with respect to va-
dard 1/2

8/124/62/000/010/013/015
Torsion of an open ... D234/D .308
rious parameters. On the basis of numerical e'x&mples.the author
determines the limits ofi 'applicability of the 'theory of thin iods
with open ptofile.,The pbbition of the center of torsion is deter-
mined. Abstracter's note: Complete translation._7
Card 2/2

.8/12 62/000/011/015/017
D234~D308
AUTHOR:
'21'21JE; Tor5ion aiid bendinG of a circular cylindrical shell
reinforced by elastic frames
PERIOD'ICAL: RefefUtivnyy zhurnal, Meklianika, no. 11, 1962, 9, ab-
stract 11V70 (In c-ollection: Vopr. rascheta elementov
aviats. konstruktsiy. no. I; M., Oborongiz, 1959,
102-141)
T--,,'XT: The author considers a circular cylindrical mom,.:ntless shell
reinforced by elastic rings and loaded at the end sections by axial
0
and tan~7ential forces. The problem of determining the forces in
the shell und the bending moments in the rings is solved in ordi-
nary trigonometrical series. For the series coefficients differ-
ence equations are obtained in which the number of the ring is the
Indeuendent variable. For a regular system of rings solutions of
the difference equations are obtained in closed fbim with various
external loads. Stressed state of a shell with elastic rings is in-
Card 1/2

8/124/62/000/011/'015/017
Torsion and bending D234/D308
vestigated in the caL3e of a 8elf-balanced force syszem a,,plied to
end sections. Tables and 6raphs illuotrate the damping of self-
balwiced stress system with increasing digtance 'from the loaded
edge. It is uhown that zhe intensity of damping depei ider
ids cons
ably on flexural ri,idity of the rings. /-A'bstracter's note: Com-
plete translation._~
Card 212

n
BOROVSMY, P. V. PHASE I BOOK EXPLOITATION BOV16 206
Konferentsiya po teoril plastin I obolochek. Kazan', 1960.
Trudy Konferenteii po teorti plastin tobolochik; 24-2~ OktYabrva
1960. (Transadtions of-the Conferenc6.on the Theory of'Plates.
and Shells Held in Kazan', 24 to 29 October-1960). Kazahl,
[Izd-vo Kazanskogo gosudarstvermogo unii raitatal 1961. 426'p.'
1000 copies printed.
Sponsoring Agency: Akademiya nauk SSSR. Kazanskiy-filiuL Kazanekly
gosudarstvannyy universitetlim. V. 1. Ullyanova-L*nina.
Editorial Board% Kh. M. Muohtarl, Editor; F. .3. liambayeva, Seorotar7;
N. A.-Alumyao'lo V. V. Bolotin, A. S. Vollmlir, N.iS.-aaniyev,
A. L. Golldenveyzer, N. A. Killchavokly, MW G. Komishin,
A. 1. Lur;lye, G. N. Savin, A. V. Sachenkov; I V. Svirskly,
R. G. Suriciii, and A. P. Filippov. Ed.: V. I: Aleksagllm;
Tech. Ed.-s- Yu. P. Somenov.
PURPOSE: Tht collection of articles is intanded'for "Ientlsts*and
engineers iho are Interested In the an-1 sis or strength ind.
stability of7ph*11i.
Cardi
1/14

Transactions of the Conference (Qont.) SOV/6206
OOVERAGEt Tho book Is a collection of artiolon dolivorod at t4*
Conforon6o on Plates and Shells hold in KazanI from 24 to 29
Octobor 1960. The artioles'deal with the mathcmiLtical theory
of platoo,and shells and I 'to application to the ablution, in
both linoar and nonlinear fomulations, of-problp=13.of banding,
static and dynamic stability, and viDration of r6gular'.and
sandwich plates and shellb 6f ftrious shapea under VarjoUj L
loadings in-the elastic and plastic regions. An4drs2u-io made
of the behavior of plates and shells in fluidsjoand the effeav
of creep of the material'is considereO. .9 ftumbo~ of-papors
discus's-problems associated.with,the developmont of effective
mathematical -methods tor..solving problems 1n -the theory of - shelli.
Some of the reports propose algorithiia for-the solution of.*probl*ms
with the aid of-electronic computers. 'A t6tal of.one,hundred,
reports and notes were presented'and discussed durIng'the con-
ference. The reports are'.arrang" alphabetically, (Russian) by
the author's-name.

Transactions of the Con.fereioe (Cont.)
Vinokurov, S. G. Large Deflections of a Conical
Panel in a Temperatura Field'
Gavrilov, Yu. V. Inveatigation of the Spectrum of
Natural Vibrations of Elsatlo Circular Cylindrical
Shells
Oavelya, S..P., and A. M. Kumemko. On the Elastic
Equilibrium of a Rigidly Clamped Shallow Shell
of Constant Curvature With Arbitrary Contour,
Galimov, K. Z. On th* Theory of Finite Deformations of
Thin Shells
Galkin 3 1 Torsion of a Circular Stiffened Cylindrical
~h a Reinforced Rectangular Opening, P%kIng
Allowance for the B-1aiticity of the Frames
oaneyova, M. S. Large Deflections of a Rectangular Plate
Under Uniform Normal 2reassure and Nor4%nLfcM,-. Heatlng
Card 5'/'14
sov/16266
66
72
77
83
92
101

L~71.22_665 Ef1P(k'j/E_NT(d1/n"'T(M )1/E'R(-'1)/_"'WP(v) Li P ( C. w/kN/0
ACC NR: AT6011759 SOURCE CODE: UR/0000/65/,000/000/0226/0246
AUTHOR: Galkin, S. 1.
ORG: None _'F(
TITLE- The twisting of framed cylindrical shell with long right-angle notch
SOURCE: Raschety elementov avlatsionnykh konstruktsly, vyp. 3: Treklisloynyye panell 1:
obolochki (Calculation of aircraft construction elements, no. 3: Sandwich panels and
shells). Moscow, Izd-vo Mashinostroyeniye, 1965, 22G-2,16
TOPIC TAGS: cylindric shell. shell dynamics, shell deformation, reinforced shell
structure
ABSTRACT: In this paper the problem of the twisting, of a circular frame-stretched
Cylindrical shell with a reinforced rectangular notch, previously discussed in two earlier
works by the same author, is generalized to apply to the case of a notch whose, length ex-
tends to 2N segments. The solution to the problem Lakes Into account the elasticity of the
transverse trusses and their discrete positioning. The skin in this case works as a ULIn
non-moment shell, receiving axial and tangential Mear forces; the Poisson factor if]
assumed to be zero. The transverse trusses continuously attached along the contour
Card 1/2 UDC 629.13.011. 1:62-43:539.4

L 37122-66
ACC NR: AT6011759
with the skin, have finite flexural rigidity in their plane and zero flexural rigidity outside
their plane. The radius of the central axis of the transverse truss Is assumed equal to
the radius of the skin midsurface. The problem Is reduced to the sotution of a system of
differential-difference equations, with the method of solution resolving Itself to the follow-
ing. At first a solution is sought to the equations for the closed part, separated from the
shell by a section passing between the trusses 1. 0 of the open part; this system is then
solved for the open part separated from the sheH by sections passing between trusses 0. 1
of the closed part. The solutions obtainedl separately for the closed and open parts are then
joined so as to satisfy the coupling condItfon3 for the--O.::th ahd 0 -th trusses located at the ,
interfaces of the closed and open parts of the skin. Orig. art. iuts: I figure and (13 form-
Ulas.
SUB CODE: 13 SUBM DATE: 250ct65 ORIG REF: 003
Card 2/2 af

ACC NRt AP7002700 SOURCE CODE: UR/0424/66/000/006/0136/0138
AUTHOR: Galkin, S. I. (Novosibirsk); Levitskaya, T. Ye. (Novosibirsk)
:ORG: none
'TITLE: Investigating the effect of frame elasticity on the state of stress in a
,circular cylindrical shell with a rectangular cutout under torsion
SOURCE: Inzhenernyy zhurnal. Mekhanika tyerdogo tela, no. 6, 1966, 136-138
TOPIC TAGS: cylindric shell, stif fened shell, weakened shell, '---qiWM4
A 5,rRF575 , 7
_7
ABSTRACT:
The results of calculating the stress distribution in a circular cylindrical
shell stiffened by transverse frames and weakened by a rectangular cutout
(see Fig. 1) subjected to torsion, are presented. The design formulas for
M A
0 Fig. 1.
I T--
4F
7~t
Card 1/2 UDC: n

ACC NR: APTq02700
such a prOD-Lem were derived previously by S. I. Galkin (Izv. Sib. Otd.
AN SSSR, no. 4, 1960; and Trudy konferentsii po teorii plastin i obolochek,
1961, Kazan'). The distributions of shear, normal, and tangential stresses
in the middle portion of the shell (in the neigiborhood of the cutout) and in
frame-stiffened portiods were calculated from these formulas on the M-20
electionic. digital computer for 38 versions of the shell structure with
geometry and stiffness parameters varying in a wide range, except * 0 - 135*
and I/R = 0.5. The calculation results are plotted in several diagrams, and
the depdendence of stresses on these parameters is discussed. The effect of
rigidity of frames, especially of frames 0, on the state of stress in the
shell, mainly on the distribution of shear and tangential stresses along the
longitudinal (reinforced) edges of the cutout and around its corners is
discussed in detail'. The different behavior of these stresses withiii the
open and frame-stiffened portions of the shell caused by the variation in
the length of the cutout combined with the variations in the rigidities of
frames, as well as the locations of maximum stresses in shells with short
and large (L0IR < I and Io/R > 1. respectively) cutouts is pointed out. A
simultaneous progressive increase of stresses (in both weakened and stiffened
portions of the shell) with increasing width of the cutout, irrespective of
the frame stiffness is noticed. The effect of stiffeners along the
longitudinal edges of the cutout on the stress distribution, and their
maximum rational cross-section areas are also examined. The dying-out of
stresses (which are caused by the presence of a cutout) in the stiffened
portion of the shell, and their practical disappearance at a distanc~e of
2 to 2.5R from the frame 0 is mentioned. Orig. art - has; 7 figures.
Card 2/2 SUB CODE*: 20/ SUBM DATE:---- 20MaY66J ogin RRF& 00'4/ATD PYMS: 5113

F. f ~ 1i 7 1 - i ; i
GALKIN S.L.
Movement of particles in a centrally -,;yrmetrir,:0 st,-itic fleld in
the aenoral theory of relativity. Izv.v!.,a -111~ Ile',- alo-304,
62 16:12)
1. 1.1,oskovskiy gosudarstvennyy universitet imeni Lomonosova.

PUFKO. V.V., dotsent; GALKIN, S.R.. assistent.
Blectrical method of igniting fuel in charging locomotive boilers.
Trudy RIIZHT iko.17:54-59 053. (MIRA 9:6)
(Locomotive boilers)

; Vill -1 ,~ :1 1 11~
GAMIN, S.R.
Calkin, S.R.
"Investigation of the Operation of Locomotive Syphons." Leningrad Order
of Lenin Inst of Railroad Transport Engineers imeni Academician V. N.
Obraztsov. Lwxingrad 1955* (Disseration for the Degree of Candidate
in Techhical Science.~
Y,nizhWa Letopist: No. 27, 2 July 1955

OATKINI T.
Adaptation for cuttlng out gaskets. Khol. tekh. 29, No 2, 1952.

1. GALKINt T.
2. US-')'R (6o0)
4. Compressors
7. Device for testing safety valves on horizontal compressors.
Khol,tekh. 29 no. 4, 1952
9. Monthly List of Russian Accessions, Library of Congress, March 1953, Unclassirled.

GALKIN, T.
V"Ives
Modernizing the Ludlow gate valve. Khol. tekh. 30, No. 1, 1952.
Months List of -Russian Accessions, Library of Congrees, June 1953. LNICLASSUMD.

.. I ~;,, t~Lltt~flt IWJ;;~ "~r, 1 .1, 11. ;
Aht~IUTIA . I " I ~ ~ , :I I I * I - ", ~
G4KP, T., glfLvnyy mekhanik.
An i=roved coupling. Khol.tekh. 30 no.2:66 AD-Je '53. (MIJIL& 6: 7 )
1. Moakovskiy kholodillnik no.q. (Gouplings)

GAMIN, T.
Oil filters of a 2-AG ammouia compressor. Khol.tokh-31 no.1:64 Ja-Kr 154.
(KLRA 714)
1. Moskovskiy kholodillnik No.q. (compressors)

.GALKIN, T.
pressors. H*'-,!.
Welding babbit flanges on pistons of horizontal corr
takh- 32 no.1:64-65 Ja-Hr 155. (MLRA 8-7)
(compressors)

GALKIN, T.
Improving ammonium valves. 1hol. takh. 32 no,3-58 Jl-- S $55.
(NIaA 9: 1)
(Refrigeration 4nd refrigerating machluery)

GALKIN, T.
.......
Improved method for the conservation of lubricants. Khol.tekh.
32 no.4:61 O-D 155- (MIR& 9:4)
(Refrigeration and refrigerating machinery)(Lubrication and lu-
bricants)

-Ts-,
Task for lubricant decantation from the oil collecting basin. Khol.
takh-33 se.2t64 Ap-Jo 156. OWU 9:9)
(Moscow--lubrication and lubricants)

SOLODOVNIKOV, P.j GALKIN, V.
Organizing the establishment of work norms in the wool and silk
industries. Sots, trud 6 no.9:90-94 S 161. (MM 142-9)
(Moscow Province-Wool industry-Production standards)
(Moscow Province-Silk manufacture-Pioduction standards)

GALKIN, V.
loot us mDre quickly eliminate ohortoomings in establishing
technical standards. Sots.trud 7 no.1:71-73 Ja 162.
(MA 15:4)
(Vologda Province-Production standards)

GALKOV, V.A., inzhener.
Increasing the efficiency of river maintenance operations. Reah.
transp. 15 no.5:23-24 My 156. (KLBA 9-.8)
(Rivers--Regulation)(Inland water navigation)

GALKIN, V.A., inzhener.
'ItORMI"WO-WOO
Correcting the settlement of a wall in the machine room of a state
district electric power utation. 219k.sta. 27 n0-5:51-52 Ny 156.
(n" 9: 8)
(7oundations)

_IALK=t_yl,%ami;."*lqksAgdrqViqh; SWILIN, P.M., nauchnyy red.; STOLTARSKIT.
L.L., red.; KAHOLOVA, V.M., tekhn.red.
[Device for assembling and welding hall structures) Prisposobleniis
dlia sborki i avarki korpusnykh konstruktaii. Leningrado Goa,
soiuznoe izd-vo sudoetralt.promyshl.. 1960. 1~3 P. (MM 13:4)
(Shipbuilding--lquipiment and supplies)
(Halls (Naval architecture)--Welding)

P M E I BOOK EX M ITATION sov/4875
Galkin, Vladimir Aleksandrovich
Prisposobleniya dlys. aborki i svarki korpusnykh konstruktsiy (Assembly and
Welding Devices for Hu3-l Structures [of Ships]) Leningrad, Sudproogiz,
1960- 133 p. 2,750 copies printed.
Scientific Ed.: P.M. Sipilin; Ed.: L.L. Stolyarskiy; Tech. Ed.: V.M. Kamolova.
PURPOSE: This book is intended for designers, process engineers, and. foremen
concerned with the design, manufacture and operation of assembly and welding
accessories. It may also be used by students at schools of higher education
and tekhnikums.
COVERAGE: The author describes devices used in the assembly and welding of ship
hull sections and discusses the purpose, classification, and design of these
devices. Methods for determining the requirements these devices must meet and
the amount of metal consumed in their manufacture are considered. The effect of
distortion welding of sections on the construction of cradles is explained and
methods are given for calculating the required number of platens, cradles, wd
Cavl-~

Assembling and Welding Devices (Cont.) sov/4875
assembly areas necessary for assemblying and welding the sections. No person-
alities are mentioned. There are 9 references, an Soviet.
TABLE OF CONTEM:
From the Author
Ch. I.. The Purpose of Assembly and Welding DevicesP Their Classification,
and the Requirements They Must Meet 5
1. Special features of assembling and welding the hull structures 5
2., The purpose or assembly and welding devices and the requirements
they must meet 10
3- Classification or devices used in assembling and welding hull
structures 15
Ch. II. Construction of Assembly and Welding Devices 18
4. Fastening and holding devices used in assembling 18
Holders 18
Clamps 20
Tightening and bracing devices 26
C &MV4/4-

S/137/62/000/005/131/150
A1601A101
AU7'HORS: M-Ikhaylov, IMI. M., Pedorenko, L. I., Myshak, bl. V., Galkin, V. A.
C
TITTIZ: Tne we'ldin- of the stainless 1 X 18H 9T (1_IQi18N19T) steel with a
tunsst.en electrode in a nitrogen atmosphere
PZRIODICAL: Referativnyy zhurnal, Metallurgiya, no. 5, 1962, 10, ~Lbstract _;,E',72
("Tr. Sredneaz. politekhn. in-tall, 1961, no. 15, 102 - IC6)
A process of welding stainless steels in N2 atmosphere was worked
out, securing not only high mechanical properties of joints, but also eliminatil-Z'
intercrystalline corrosion.. All test pieces were butt-welded with the help of
a HXAYI AP+3B (NIA-M JM+3B) torch. The experiments yielded the follo'wirz, re-
sults: 1) the main, difficulties during the arc-weld-Ing in N2 with a '.-I-electzodc,
such as the bullYoling of the bath, seam porosity and the high consumption of elec-
ro"es, are not caused by the disintegration of unstable W-nitrides, but by the
presence of 02 in 'Une arc burning zone. 2) The are-welding in N2 with a 'W-elec-
trode takes a normal course and secures a high-quality seam in case N2 does not
contain more than 0.2% 02. 3) A waste of C is noted during the are-welding in
Card 1/2

The welding of...
S/137/62/000/005/13-1/150
A1601P,101
with a W-electrode. This is a decisive factor for decreasirlG- tile tendency
01- the seam to inte'rerystalline corrosion. 4) The are-welding in N2 increases
- 4
the efficiency of the process by 30% amd decreases labor costs 15 times In COT.1-
parison to argon arc-welding. The arc-welding in N2 does not deteriorate the
qualities of the products.
V. Tarisova
[Abstracter's note: Complete translation]
Card 2/2

GALKIN, V.Ikl-
(;o.U.e(-.tive of cowunist labor. Pat' i put.khaz. 6 mo.5.39
16,2. (0bl 1514)
1. Zamestitell nachal2nika Krichevukoy distantaii Belorusakoy
dorogi. (Railroads-1hployses)

I
GALYM,, V.A.
Brigade method of operating ring spinning machinery it wool cloth
manufacture. Tekst.prom. 22 no.4!5-7 Ap 162. (MM 15?6)
1. Nachal2nik otdela truda i zarabotnoy platy Upravleniya sherstya-
noy i shelkovoy promyshlennosti Moskovskogo oblastnogo soveta.
narodnogo khozyaystvao
(Woolen and worsted spinning)

CALIKINJI V.A., inzh.
Redesilning and testing of a hydraulic piston compressor.
(Trudy LMZ no.10:310-314 164. (MIRA 18:12)

Q , Y, V, - -A,.-
"AIAL-, I IP1.
N15
6",
.G1
Mekhanizmy patologicheskikh reaktsly L Nechanizma of pathological reactionsj
Leningrad. Medgis. 1955. 498 P. Illus., Tables. Includes Bibliographies.

G?,L,i,,, V.
in HyTori-olli,c Di,--~' Firqt "loscow CYcler
Inst- r'oscow, .1955 (Djs~;ertatlon f~r dr-Cre-? of* Cand-
d!Rt,~, in X-dical 3-3clence)
-90: hnizlim--ya IctollA31 No. July J,Qr~,~

wALKIN, V.A., kandidat meditsinek-1kh nauk
Bloodletting by venesection and leaches in hypertension. Terap.
arkh. 28 no.4:16-23 156. (XLRA 9:9)
1. 1z fakulltetokcy torapevtichaskoy kliniki sanitarno-gigiyeniche-
skogo fakulitets (dir.-prof. A.G.Gukasyan) I Noskovskogo ordena
Lenina maditsinskogo instituta iment I.M.Sechenova.
(HYPIW=SION, Aher. -
blood letting & blood extraction vith leeches)
(LMEMS,
ther. use In b7pertension for blood 16ttir4)

GALKIN, V.A.
--l-~,;1-uretic qualities of small doses of mercusal in cardiac decompenra-
tion. Sov.md. 21 noe9:54-56 3 157. (MIRA 11:1)
1. Iz fakul'tatakoy terapaytichaskoy kliniki s& nits rno-gigiyenichs-
skogo fakuliteta (zav. kafedroy - prof. A.G.Gukasyan) I Moskovskogo
ordena Ienina meditsinskogo institute imeni I.M.Sechenova.
(DIURUTICS, ther.ume
mervelyl theophyllinate in congestive heart failure
Otus ) )

GALKIN, V.A., inzh.
Improving sanitary conditions in welding shape. Bezop. truda
v prom. 2 no.1:30-31 Ja '58. (MIRA 11:1)
(Blectric welding--Safety memsures)

IVANOVA-FEZNAMOVA. A.Tu. dots,', GALKIN, V.A. (Moskva)
Use of BecurinIne in internal diseaseee Ilin,med, 36 no,9:135-137
S158 (MIRA 11:10)
1. Iz fakulitetskoy terapevticheskoy kliniki (dir. - prof. A.G.
Gukaayan) sanitarno-gigivenicheakogo fakulltata I Moskovskogo ordena
Lenina meditsinskogo instituts, im. I.K. Sechenova.
(AT-YA IDS, ther. use
socurinine in hypothenaion (Rus))
(HTPOTKNSION, ther.
securinine (Ru))

GALKIN, V.A.; CHECHULIN, A.S. (14oskva)
fterimental production of cholecy8titie. Pat.Aliziol. i eksp.
terap. 3 no-1:78-79 J,%-F 159. (MIRA 12:2)
le Is TSentrallnoy nauchno-looledovatellskoy laborntorii im.
S.I. Chechulins I Mookovskogo ordena Lenina meditsinskogo insti-
tuta I.M. Sechenova.
(CHOIZCYSTITIS, experimental
induction (Bus))

ARKHANGELISKAYA, GRIGORENKO, R.V.; LKVTOVA, K.Z.;
CHECHULIN, A.S.; GARVEY, N..N., red.; RA7K0q N.M.p takhn.red.
(They serve the motherland; tenth anniversary of the graduation
of pbysicians at the I.M.Sechenov First Moscow Medical Institute
in 19491 Oni alushat Rodin*; k 10-letiiu,vypuska vrachei 1-go
MOLMI imeni I.M.Sechenova 191+9 g. Moskva, 1960 81
(M& 14:6T&
(MOSCOW-MEDICAL COLLBGBS)

"~~ ~V.A. _--
Use of neodicoumarin in myocardial infracts; clinical and
experimental observations. Terap.arkh. 32 no.1:18-23 Ja
160a (MIu 13 110)
(HRM-nUqWTION) (C=AM)

LK~I,-V.A-.-,kmid.med.nauk (Moskva)
_T~
Public health in the Kingdom of Yemen. Sov. zdrav. 21 no.3:
79-82 162. (MIRA 15:3)
(=N-PIJBLIC HEALTH)

GALKIN, Vaevolod Aleksandrovich; LAZAREV, M.S., otv. red.;
-I--,. ~ - -
01
OV, V.V., red. izd-va; MIKaINA, L.T., tekhn. red.
(In Yemen; Soviet physician's notes) V Iemene; zapiski so-
vetskogo vracha. Moskvra, Izd-vo vostochnoi lit-ry, 1963.
104 P. (MIRA 16:9)
(Yemen--Social conditions) (Yemen-Public health)

GALKIN, V.3evolod Aleksandrovich, dots.; GUKA,9AII, A.G.) prof.j
- -I-..- ".... ---- zaq]L-; ~ ddyatel I nauki, red.
[Cholecystitis in the clinic for internal diseases] 0 kho-
letsistitakh v klinike vnutrennikh boleznei. Pod red. A.G.
Gukasjana. Moskva, 1-i Mosk. med. in-t, 1963 108 p.
~MIRA 17.2) i.
1. Zaveduyushchiy fakulltet~;koy te,--apovtichoskoy klinikoy
sanitarno-gigiyenicheskogo fakul'teta Moskovskolro meditsin-
skogo instituta imeni I.M.Sechonova (for GU-asyan).

GAIKIN, V.A. (Moskva)
History of the stady of clinical aspects of'ohronic alcoholism.
Trud~ Goo.. nauah.-issl. inst. psikh. 38tIf42-4,48 163
(MIRA 16:11)

GALKIN, V.A..
Some aspects Of the nutritirx J thz~ p--pulafl;-11 -f Ye:acn.
Vop. pit. 22 no.3:82-831 My-.c 163. (!,'; " 11 '. 17,-, 8)
a. lz kafeciz-y fakull T.-. r a p-: I k~,,av . - p~-, I' ~ *-G. Giikatyan)
~ . . :~ K .'-' L C) .4
sanitarne-gi glyen, cheskz.,-c, . f akul I -ze ta 1 11('..% ' , rd na
It en-na med' ts- nskcgo ino t~ ~ -,en ` I P. S.
I - . - - I

Appearance of pathological liver changes in experimental
cholcc~atjtjs. Pat. fiziol. i eksp. terap. 8 no.4168 JI-Ag 164.
(MIRA 18,-2)
1. r-entral,naya nauchno-issledovatellskayg laboratoriya Imani
Chechulina (zav. A.S. Chechulin) i kafedra fakulltetskoy- terapil
sanitarno-gigivenicheekogo fakullteta (zav.- prof. A.G. GukasYan)
I Moskovskogo ordena Lenina instituta gematologli i perelivaniya
krovi (dir.- dotaent A.Ye. Kiselev) Moskva.

, ~-ev(
--l , - -,led liel-oandrovich,
[Soviet pIrysivians in Ycr:.en ,I Sovetskie vxracEi v lampme-
M
oskva, toleditsina, 1964. -; ~ P. I ~
I (!~'I; A 17: 5)

GALKIN, V.A.
Development of the clinical views of Moscow psychiatrists
in the 19th century; pre-Korsakov period of the Moscow
school of psychiatrists. Trudy 1-go MSMI 34:74-821 164.
(MIRA 18:11)

CALKIN V,Aq TAF.,)SOV, K.Yeop dcts!~-,lt
- j
Sigr,-'fl-,anr,e of thr nlassificati~m of disease.9 ~n d.i.-agnovis.
Trudy 3--go MMT 372157-163 Q5.
(MIRA 18;8)

SOBDI-rlv, V.Ft.; GAMIN, V.A.,- BROblNOVA, N.S.
Expedient methods for the administration of tetracycline JLn
treating chronic cholecy-Aitis. Antibiotiki 10 no.2:173-176
F 165- (WRA 18:5)
1. Kafedra mikrobiolo ii (Zav deystvitellnyy chlen ARN SSSR
prof. Z.Vjermollyeva~ T.Sentrallrogo instituta usovershenstvovaniya
vrachey i kafedra fak-ul"Itetskoy terapii (zav. - prof. A.G.
Gukasyan) I Moskovskogo ordena, Lenina meditsinskogo instituta
imeni Sechenova.

MASLITEEV, A.T.; GALKINp V.A.
Results of using hypnosis in the treatment of dy9kinesias of
the biliary tract. Trudy I-go MMI 34:464-470 164.
(MIRA 18:11)
1. Kafedra psikhiatrii (zav. - zaaluzhennyy deyatell nauki
prof. V.M. Banshchikow); kafedra fakulltatskoy terapil sani-
tarnogo i vechernego fakullteta (zav. - zasluzhennyy deyatell
nauki prof, A.G, Gukasyan) 1-go Moskovskogo ordena Leninft
wditsinakogo instituta imeni Secherova.

GALKIN, Viktor Dmitriyevich; OBIDAROV, Vasiliy Nikolayevich; KEZIVETSKIT,
DUMAYN, P.P., kand.tokhn.nauk, red.;
MOROZOVA, M.N., red.isd-va; DOBRITSYNA, R.I.. tekhn.red.; GOR-
DBYNVA, L.P.. tekhn.red.
(Effective dimensioning and indication of tolerances in mechanical
drawings] Hatsionallnais prostanovka rasmarov i dopuskov na
charteahakh. Moskva, Goo.nauchno-takhn.isd-vo mashinostroit.
lit-ry, 1960. 150 p. (KIRA 13:7)
(Mechanical drawing)

GALKIN, V.G.., inzb.
Effect cf the d67!a--ion of com. pAr&Tnet.0ro of it torm
tion 0
on the changes In. the va.~Lua of the r-bactive electromotive fcrce.
Trudy MITT 4Oz99-IU 363. OIC RA 18 18)

GALKIN, V.I. (Moscow)
ASD therapy in pulpitis. stomtologita, no.6:18-21 '53. (XLU 7:1)
(Tooth-Diseases) (?issue extraots)

LYAKH V.M. inzh.; GALKIN ~Z, t
.9 Y I t, 1.
Results of testing new b-3et calUvators. Wkh. i elek. sots.
sellkhoz. 21 no-4:53-57 163. (MJRA 16:9)
1. Ukrainskaya mashinoispytatelinara stantsiya.
(C~Itivators)

--~GALKIN V.G. (Petrozavodsk)
Physical development of Petrozavodsk school children and methods
for improvement in the light of now problems. Sov. zdrav. 19 no.6:
51-55 '60- (KIRA 13.9)
(PETROZ&VODSIZ-CIIILDRM-..OROWTH)

GALKIN,."L,P., inzh.
Method for the control of the position of the neutral in MB-406
traction engines. Elek. i topl.tiagn no.8s27-28 Ag 163.
(MIRA 16:9)
(Electric railway motors)

GAIMO Y.G., insh.
I .-,:- --z-~----'.
76ating of a.c. machiness Elek.i toplotiaga 7 nools2445 Ja 163o
(MM 16927
(Rectric pachftery-T"ting)
(ILectric locmotlvq;;z anoo and repair)

GAMIN V.6,4Qhlta)
-~~Ow
Slow consolidation of a fracture of the shin in a patient whose
spleen has been resected. Ortop.travm. I protez. 17 no.6:117
Y-D '56. (MLRA 10:2)
(TIBIA-FUCTUBS) (SPIAN--SURGERY)

Gki"To V.I.
ice tbrttoU onto the obores of lake Baikal, PrIrO4 30 zkoolt82-83
Ja 161* NMA IASI)
:L,, BoWkaltakV& 1-1 logicbeakAWs, stautelyao
(Ba4ko'l Ldkt-loe w rivwat Waft stcp)

GALKINI V. I.
~ tz2mi rp-w--"
Glaciation on the banks of lake Baikal. Trudy VSGI SO AN SSSR
n0.3:50-59 161. (MIRA 15C10)
(Bmikal?; lake-Moraines)
I
i

LEBEDIK, A.I.; --qAIM,,V 1.; ROGINSKIY, G.I.; BUDIKO, V.A., red.; GURF,
VICH, M.M., tekhn. red.; TRUKHINA, O.N.p tekhn. red.
[Work like Vladimir Siretlichriyi does] Rabotat' kak Vladimir Svet
lichnyi. Moskva, Izd-vo sellkhoz. lit-ry, zhurnalov i plakatov,
1961. 70 p. (MIRA 14:11)
(Sugar beets)

LEBEDNIK, A..L; GALKIN, V.I.; ROGINSKIY, 0.1.
-------
[Work as Vladimir Syetlichnyi does]Rabotat' kak Vladimir
Svetlichn.vi. Kishinev, Partiinoe ltd-vo TeX X? Holdavii,
1962. 48 p. (MIM 16:3)
(Sugar beets)

DUDKO) A.I.- GALKD-1 V.I.: YEGOROV, G.A.; ]NITRIYEW, I.E.., red.;
red.; DEYEVA, V.M., tekhn. red.
[School of Vladimir Svetlichnyi] Shkola Vladimirs Svetlioh-
togo. Moskva, Sol Ikhozizdat, 1962. 95 P. (HIRA 15-.7)
(Sugar beets)

"A~LN,_-V.I. .,[Halkino V.I.]
One centner of sugar 1xiets requires 13,, 4 man-minutes. Mekh.
sill. hosp. 13 no.4:3-5 Ap t62. - (MIRA 17:3)
1. Rukavoditell laboratorii Kubanakago nauctino-issledavatellskogo
instituta ispytaniya mashin.

GA11111, V.I.; MARKOV, N.N.
A
Auger core drilling without lifting the auger string. Trudy '-'.vB
no.5:82.-87 162. (MIRA 180',

GAMIN,, V ~il~ , inzh.
Cb.amgcA in the ground water cycle at industrial sit-a-ij. Fxoit.
stroi. 39 no.ll-,IS--~-19 161. (HIRA 14,,,,12)
(Water, Underg,ound)

~. I , !'.' ~-*~'. T- , 7 , ~ j, ! - -~ ~- ~ ~--. r
; .:, . '. I ~ -; I ,. , . , , , Y.
, r i.-21 i 117 Ir-I I,, I iv 11, (-: ~ ,, , i n /?l " - I - - . - I .
New for bu~ Ild ingi of p synthe , 4 - rubber plart. Frcm.
stroL 42 '65. (VURA. 1e; 3)

1210
AUTHOR; _Salkin, V.S._ (Moscow)
2'_,~ 2 65
S/179/61/000/003/003/016
E031/E435
TITLE- rhe ln-`-estigation of the hypersonic flow round a flat
Plate in a viscous rarefied gas
PERIODICAL; Akadewl~-Ya nauk SSSR. Izvestiya. Otdeleniye
tekh-n1cheskikh nauk. Mekhanijza i mashinostroyeniye,
196'1, NQ-3, pp.18-21
TEXT. -rh e~~.&I,-_-ulation of the drag ;oefficient of a semi-infinite
flat plata wh.1~.h _e thermally isolated in a !-.typersonic gas flow
ith zlip 1-t -J*Z-_-1h=d. It is assumed that the domain of the
flow betwsen ~hEt .5L-'_-ac:hed strong sh.~_-k and the plate consists of
-1 in is A strong
-n i -v-- ._-id zone and a laminar boundary layer.
interac-,,_ion bet-wear-, the shock and "the boundary layer is postulated.
Then the affac-,; of alip and the tempera`o:ure discontinuity in the
region `_-he bix-,nziary layer eqi.~ati~:,ns are applicable is only
-5ignlflc~ant in the of a strongly heated plate. As the
P-JO, vu.0being the macroscopic velocity and c the most probable
;.I-
Card 1/2

S/124/62/000/002/002/014
On taking into account the ... D234/1)302
velocity of thermal motion of the molecules) the air can be considered
as a single-component gas with the same density, temperature and mean
molecular weight.. The investigation is carried out under the condition Vil,
of diffuse reflection of the particles from the body and the coefficient
of accomodation cLL~ 1. i-Abstracter:s note: Complete translation] -
Card 2/2

AUTHOR-. Galkin, V.33.
143145
5/.124/62/000/008/005/030
1006/1242
TITLE: Tile limits of applicability of the relaxatio.n model
of Bol-?in-ann's kinetic e4uation
I'SIRIODICAL; liei'erativnyy 7hurnpl. Mekhanika, no.8, 1962, 22
abstrnct 8B134.
(fnzhenernyy zh., v.1, no.3,
1961, 153-156)
TEXT: In the solution of proble.ms bf aerodynavics of r.-.re-
fied gases with the aid of Bol7mann's kinetic equation, eTent*
difficulties are encountered due to the complicated form of this
equation. Simplified models of Bol9nnnn's enuation are therefore
'frequently used, the simplest being the relaxation model ~Lf . fO-f
dt T
Card 1/3

S/124/62/000/008/005/030
10061"1242
The limits of applicability of...
where f- the unknown~distribution function, fo - the Fax-well dist-
ribution function, r - relaxation time equal to 11 /p ( it, - viscosity
coefficient', p - pressure). In this work the limits of applicf~bili-
ty of the relaxation model are illustrated by the ex,~mple of a gas
slip flow. Ifere the Gas slips along a plane in one direction r-nd a
constant gradient o1 Ule mucroscopic velocity u, parallel to the
plane, is maintaLned in the y-direction, perpe-ndicullar to the plane:
du/d,v = const. The syotem of equations of kinetic moments, de-rived
from the relaxation equation, is solved for this purpose, and this
solUtion is compared with the known solution of the exF,.ct system
of equations of kinetic moments. Only moments of third order parti-
tion functions Qijk are considered. 'The equations of kinetic mome-
nts are obtained by multiplying.the equation by thie product'of a
Card 2/3

10,1000
S/040/61/025/006/0101/021
D299/D304
AUTHORS: Galkin, V.S., and Gladkovp A.A. (Moscow)
TITLE: On the lifting force at hypersonic speeds
PERIODICAL! Prikladnaya matematika i mekhanika, v. 25, no. 6p
19619 1138 - 1139
TEXTs It is established that the lifting force of many types of
bodies (wedgest conea# etc.) is negative at hyperiqonic speeds for
any values of Knudsen's number and for any angle of attack a (O-zz,
-Z-- a mEj; V12). A very simple case is considered: Pree-molecule flow
past a wedge with semiangle S; the flow velocity V -:~-c, i.e. S = V
/ where c is the most probable thermal velocity of the on-
coming molecules. The lifting force of the wedge is
Y ;~~sin 2a cos 28 for 8 >-a, Y,;:~ sin 2(8--a)
for 8