SCIENTIFIC ABSTRACT FILIPPOV, G.G. - FILIPPOV, I.N.

• Document Type: CREST
• Collection: Scientific Abstracts
• Document Number (FOIA) /ESDN (CREST): CIA-RDP86-00513R000413120001-9
• Release Decision: RIF
• Original Classification: S
• Document Page Count: 100
• Document Creation Date: November 2, 2016
• Document Release Date: June 13, 2000
• Sequence Number: 1
• Publication Date: December 31, 1967
• Content Type: SCIENTIFIC ABSTRACT

.89207
S/056/61/040/001/013/037
The interaction between B102/B204
tainedg the electric field-is characterized by the intensity of the plasma
waves. Aceordingly, the velocity modulation of the beam and a subsequent
clustering cannot be described by means of this system of equations. Fi-
nally, the dispersion relations for a steady linearized problem concerning
the growth of a plasma wave inteneityare solved and a theoretical - experi-
mental comparison of the range of linear slowing down was carried out. All
that has been said is based upon the assumption that the density of the fast
electrons is considerably lower than the plasma densityt and that no exter-
nal electric or magnetic fields exist. The authors thank V. S '. Imshennik,
Yu. I* Morozov, E. Z. Tarumov, and V. A. Teplyakov for discussions; L. P.
Strotseva and M. P. Bronnikovs, carried out calculations. There are 16 refer-
ences: 9 Soviet-bloo and 7 non-Soviet-bloo.
SUBMITTED: May 6, 1900
Card 3/3

FILIPPOV G.G.
Selecting the working conditions for separation processes*
Trudy ICHTI no.40:113-115 163.
WIFA 18:12)

NAUMENKO, M. F.; DELEKTORSKIY, N. V.;,tWILIPP~V, ... G. G.; AVERBAKH, K, I.
Information. Khim prom no. 3:234-237 Mr 164. (MIRA .17:5)
vg,~,

FT1".-,-`OV G*G.1- SAKCIDIT'SKIY, K.I.; "FLIVEINSKly, YaJ,'-
I I I
Use of the effective concentration methord for ca1c,,:1atin1g the
dual temperature separation of Isotopes. K-him. prom. 4-1 no.1:
10-14 Ja 165. (',~jj~--,A 18:3)

FILIPPOV, G.M.,
Propagation of electromagnetic waves in a laminated medium.
Radiotekh. i elektron. 9 no.3:547-551 Mr 164. (MIRA 17:4)
A" A' .,-- . I

---F'LLIPPQI, - G.G.
Adsorption equilibritrn and Poissons distribution. Zhur. fiz. khim.
39 no.2:305-306 F 165. (K[RA 1814)
1. Fiziko-khimicheakiy institut imeni Karpova, Moskva.
~lq

i On il., t, mi ,.i1 ty Li the br i-gadao anc! c-ein of
C~ amnZi I b L1Qym -~n :.vaijaportation. Trudy MVT no.498
31.-,4() 'f4 4;.l.'RA L8 12

--FILIPPOV-G---S--and-GCPOli7I'IS"'VTASOVA~-L. -M.
"Bacteria in Match Induatry, " Zhvr. I-licrobiol., .11, 11 6-11, 1930.
lab. Hyg., Bact. Inst., Dnepropetrovsk.

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inzh., red.; FZVZNKR. A.S., zav.red.izd-va; MELINICHWO,
F.P.. takhn.red.; TETYMNAN, T.K., tekhn.red.
[Production norms for planning and reeenrch work paid by the piece-
work system] Normy vyrabotki na proaktnye i izyakatellskie raboty,
oplachivaemye adallno. Moskva, Goe.izd-vo lit-ry po otroit., arkhit.
i stroit.matarialam, Pt.17. [Lumber and woodworking industries]
Lesozagotovitallnaia i derevoobrabatyvaiushebaia promyshlennost'.
1958. 39 P. (MIRA 13:1)
1. Russia (1923-- U.S.S.R.) Goeudaretvennyy komitet po delem stroi-
tel'stva.
(Lumbering) (Woodworking industries)

I-() V, -Z~-
POSE I BOOK ECPLOITATICK SCF/3707
Vaeillyev, Dmitriy Vasil 1.1revichP and Gleb SergeyevIch F121ppov
Oanovy teorli i rascheta Gledysshchikh sistem (Pundamentals of Theory and
Design of Servtay3tems) Moscow., Goaenergoizdat, 1959. 428 p.
220000 copies pnnteu. Errata slip inserted.
Ed.: Yu. A. Sabinin;. Toch. Ed.: Ye. Me SobolovRe
PUR111WE: 7his textbook vas*approied by the Ministry of Higher Education, USSR,~-'--
for elecl;rical engineering and power engineering schools of higher education.
It may alio be of i use'to engineers dealing with . problems of autmation
COVKRAGE: The aulthors present the fundamentals of theory and desigaof servo-
systems both in a linear approximation and also vith noallnearities taken
into a4count. Methoas of Improving the quality of servo-Syste-m performance
are discussed, and typical circuit diagrams of servosystem used in engineering
practice are presented. The book was written in accordance with the program
of the course on serircsystems at the Leningrad Electrical Engineering Institute
imeni V.I. Ullysnov (Lenin) for students of various specialities. 'The authors

YundAmentals of Theory (Cont . SOV/3707
thank V.S. LevitY senior teacherX for his help. There are 37 references,
all SovIet (8 of these are translations)
TABLE OF CONTENTS:
Foreword
3
Ch. 1. Introduction
1' Basic -concepts mad definiti 0
'on 11
2: Develolment of slervomyviems
and fields of their application 17
3- Classification of,systoms of autmatic coutrol Emd.of servo-
systpm 22
Ch. II. Principal Varl.etieo and Structure of Servcsyste=
1. General characteristics of the principal varieties of
.errosylste"
2. Typicu.L equivalent sections and block diagrems of serv~-syatems 31
A. Typical equDmIent sections 3i
1.~ Inertialeas section 32
2. Aperiodic section 33
3- Integrating section 34
";z1-

4
88714
AUTHORS:
V5111 2"
Shullgal V. I.,Engineer, Bekushev, V. I., Engineer,
_j20vj Go Sep Engineerp and Kuzlmin, V. M~t Candidate
_fAji
of TeoRnical Sciences (Leningrad)
S/127/60/000/006/001/007
B012/BO54
TITLE: Test Results of the BAW-250 (BASh-250) Drilling Unit
PERIODICAL: Gornyy zhurnal, 19609 No. 6, PP- 39 - 43
TEXT: The SAM-250 (BASh-250) drilling unit was designed at the institut
Gipronikell (State Design and Planning Scientific Research Institute of
the Nickel; Cobalt, and Tin Industry), and built by the test plant of the
Institute (in the third quarter of 1959). The first testing stage was per-
formed at Priozersk, Leningradskaya oblast' , in the fourth quarter of 1959.
The results of this test are described. The second and final test will be~
made in the third and fourth quarters of 1960. Vertical blast holes were
drilled in red granite with a hardness of 14 - 16 according to Protodl-
yarkonov, 21 m deep,:at a distance of 3 - 4 m from the bench edge, Rolling
cutters 214, 269, and 300 mm in diameter were used. The 21,t n-n cuttEmoftye
Card 1/3

88714
Test Results of the 6PI-250 (BASh-250) S/127/60/000/006/001/007
Drilling Unit B012/BO54
Povarovskiy zavod VNIIBT (Povarovo Plant of the- All-Union Scientific
Research Institute of Drilling Technique) and the 269 mm, cutters of the
Kuybyshevskiy mashinostroitelfnyy zavod (Kuybyshev Machine-building Works)
were armored with cylindrical teeth of'j;K-8'n (VY-8V) cemented carbide with
spherical working surface. The 300 (295) mm rolling cutters were armored
at the zavod-Ceopribortsvetmet (Geopribortsvetmet Plant) with cylindrical
teeth of-m.K-15 (VK-15) cemented carbide with chisel-like working surface.
Compressed air was supplied to the drill hole by thr e mobile AK-9 (DK-9)
Diesel compressors, each with an output of 8-5 - 9 mi/min at anoperational
pressure of 6 atm cxcess-pressure. The essential technical data of the
unit are: drill hole diameter 250 mm, drilling depth 22.5 m, tool feed:
rope-hydraulic, chisel: three-cone, axle load: 25 t, speed of tool: 0 -
150 rpm, lifting speed: 4 m/min, tool feed: 0 - 21 m/h, removal of fines
from the hole: by compressed air, specific pressure of caterpillars on the
11
ground: 1.23 kg cm', weight of the unit: 50 t, number of operators: 2. The
test reEP_&ts.dXViq1 at'tie drilling rate attained the 1.2 - It .8 fold with the
269 mm chisel, and the 1.4 - 1.8 fold with the 300 mm chisel, as compared
Card 2/3

88714
Test Results of the;-).-, -250 (BASh-250) S/127/60/000/006/001/007
Drilling Unit B012/BO54
to the 214 mm chil3el. When perfect supports were available, all chisels
proved to be suitable even when 50ro of the teeth were missing or worn out.
Some drawbacks were found which are to be eliminated until the second test.
It is stated in conclusion: With the drilling unit under review it is pos-
sible to drill holes in rock with a hardness of 14 - 16 at an average out-
put per shift of 24 m. It is convenient to use the unit for drilling holes
with rolling cutters,.250 - 300 mm in diameter. The rolling cutters men-
tioned are intended for drilling under scavenging, and therefore show
little durability. There are 1 fi6nire and 3 tables.
ASSOCIATION: Institut Gipronikell Leningrad (State Design and Planning
Scientific Research Institute of the Nickel, Cobalt, and
Tin Industry, Leningrad)
Card 3/3
'F-E "I

FILIFFOV,-G.S.,, insh.
Drilling with a roller bit in flooded strat4.
Gor. zhur. no.6:38-39 A 162. 1 (MM 15:11)
1, GosWarstvennyy institikt po proyektirovaniyu
'predpriyatiy nikelevoy promyshlennostil Leningrad.
(Murmansk Province-Boring)

Up/
EO)K FXPLOITATIU-1
Labor, Laureate of the Prize); IL
(Flerc of Socialist
indt~slrial bitildings -ini,,r -ozezi ground
ri I I ruc i Ll -u:-,
Tn Jeal-)
urit" FS-6 wn Q f-, 1 c r
4W
13
Pn P.NV

F]; 48264mw
The is intend-ad for engineering and tachni.cal workers q~4alifted for the
~~>niit.ructl,on ,,)rk in the axeas of pennanently !rozen ground.
'j'ARI-F OF (atridged)i
I LLLn
E.7
~7~7- -N
21
M,oj ~
uct ;,,)n
En,-,-Ineetring and geological exploration ond proz--pi!-ati-ng
eparation of tie territcry GLr~,--
c-ring pr
constrjct~.on methods u;]r-,-
i on pec~i-liaritipam of s,.LrfP-,-e e s c. n CT, t T;t
!ps-vinnently frozen ;rrounln
f4 r t 1~ j C -LOWS. tt, ,:r, j I
-a t ion )f Dlumbing and h-L-a t ing
M E
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U., -1 RMN I
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; 1. 3/3
~ - -C.rd

FILIPPOV, G.S.
Single-Ltyer asphalt ccncrete pavements in northern reCicna"
Avt.dor. 24 no.9:7-8 S 161. (MIRA 34:10)
(Pavements, Corcrete)
PR

KUZNETSOV, I.K.,, Geroy Sotsiali8ticheskogo truda, laureat
Goaudarstitennoy premii; FILIPPOV, G.S.0 in-h.;
EMZOVSKI-Y, B.I.1 kant room-. red.
[Building industrial structures on permanently frozen
soil] Stroite'llstvo promyshlennykh sooruzhenii v uslo-
viiakh ve(-,hnomerzlykh gruntov. Moskva, Stroiizdat
1964. 210 p. (~aRA 18:21

FILIPPON-2-G.V.-- --(Deceased)-----
(Mechanical Engineering)
See ILC

-FILIPPOVIG.V.
Profiling the inlet section of a channel according to a given law
of pressure changes along its axis. IzV,vys,ucheb.zav.; av.takh.
5 no.108-40 162. (KRA 16:7)
1. Kuybyshavslciy aviatsionnyy institut, kafedra aerogidrodinamiki.
(flydrodynimics)

BONCH, E.I.; XUZIMNAI, Ye.A.1 FILIPPOVp GOV.
Using aerosols in forests. -Zashoh. rest. ot vred. i bol. 8
no.2:23-24 F 163. (MIRA 160)
(Spraying and dusting in forestry)
"P-11,

32266
B/612/59/000/008/005/016
24-4'~ 00 D216/D304
AUTHORS: Kudryashev,' L. I,, Doctor of Technical Sciences, Pro-
fessor, and Candidate of Technical
Sciences
TITLE: On the composite boundary layer at the entry region
of a circular tube
SOURCE: Kuybyshev. Industrial'.nyy in8titut. Sbornik naucl-mykh
trudov. No. 8, 1959. Teplotekhnika; voprosy teorii,
rascheta i proyektirovaniya, 61-66
TEXT: The authors consider .the problem of the position of tile
transition point from laminar to turbulent flow for the boundary
layerp and the effect of Reynolds number on the total coefficient
of resistance. The coordinate of the transition point is deter-
mined using the idea of a critical Reynolds number and L. Shiller's
theory of the laminary entry region. Assuming a parabolic velocity
distribution in the boundary laminar layer at the entry,
Card 1/ 5

On the composite boundary
f
Re- T
2 '.4 6 ---16-
-V 1+
where u V,
vav ay Re vay 0
(2)
where vx velocity in the boundary layer, U - velocity in the cen-
ter of the flow, v av.-. mean velocity Z-Abstractor's note: 1 unde-
finedj, The distance x from the center is relative to the radius
.of the tube r00 The quantity Re x is considered, where v av and r 0
32266
3/6ly59/000/008/005/016
D216 D304
Card 2/ 5

32266
B/612/59/000/008/009/016
On the composite boundary ... D216/D304
are replaced by U and x respectively. Then, using Eq. (1)p the va-
lue of Rex at the point of transition is
Rext =1 1- f 1 + It) Re2 =T(4&)Re2 (5)
4
Since the boundary layer is least stable in that cross-section
where its thickness is greatest, and where the negative pressure
gradient is a minimum, i.e. at the end of the entrance regiong
then through Shillerg Re = 3.04.1o5. Thus, for a fixed Reynolds'
xt
number, the value of Itt may be determined, and the coordinate of
the transition point x, is given by
x 3,04#105
t Re ( I +4~) (7)
Card 3/ 5

On the composite boundary
32266
S/61 59/000/003/005/016
1)216YI)304
To determine the relative thickness of the laminar and turbulent
boundary layers, the hypothesis of equality of thickness of momen-
tum loss is used. This is determined for the laminar layer by
1 4N =.091333'~l - 0905 1 2
t t t
(8)
and analogously for the turbulent layer. Then, the overall length
of the entry region and the field coefficient K = Vav /U may be cal-
culated. The total resistance coefficient k is given by
Po P I
Ao d
Pv av
(9)
Card 4/ 5

32266
S161 59/000/008/005/016
On the composite boundary ... D216YD304
where 1 and d are the length and diameter of the tube, and p and
are the pressures at the entry and end of the region cons'dered
7Abstractorls note. p undefined. 7. The ratio of this to the re-
~
sistance coefficient Tor hydrodynHmically stabilized motion for 1
less than the length of the entry region is calculated and for
Re = 40009 this ratio is I. Increasing Re produces a sharp drop,
reaching a minimum at Re = 5000. After this, the ratio rises slow-~
1y, reaching a limiting value analogous to the value for a purely
turbulent boundary layer at the entry. For apparatus, in which
the Reynolds number is close to the critical value, the authors
recommend that the possibility of chafiging it during operation' : I
should be examined, since -the total resistance coefficient depends
strongly on it. Alsog to increase the heat exchange apparatus, with
the Reynolds number in the range 2,300 - 10,000, the flow at the_
inlet should be turbulent. There are 2 figures, 1 table and 3 So.
viet-bloo references.
Card 5/5

S/147/62/000/001/od5/oI5
E195/E135
AUTHOR: Filippov, G.V~.
TITLE: Calculatin~_the form of the inlet section of a
channel according to a given law of pressure change
,.along its axits.
PERIODICAL,. Izvestiya vysshikh uchobnylch zavedeniy,
Aviatsionnaya tekhnika, no.1, 1962, 38-40
TEXT: The author provides a solution to the problem of
calculating the profile of an axially symmetrical channel, which
is considerably simpler than the One originally developed by
V.G. Sanoyan. The problem is simplified by the use, as a flow
model, of the highly expanded diagram in the inlet section
(see Fig.1). The solution is dependent on a-number of
assumptions: firstly that the velocity profile at the inlet is
uniform, that the inlet section consists of boundary layer and
streamline flow (ACB) zones, that in the streamline zone the
velocity remains constant along the cross-section, and lastly
that the axial pressure gradients are small-and consequently
channel walls are curved gently. Reducing his problem to a
Card 1/3

Calculating the form of the inlet..$ S/147/62/000/001/005/015
E195/EI33
two-dimensional slit, the author obtains the final equation for
h as folloys: Vavero
h U - ho + 6, (3)
The displacement thickness 0' can be determined from the
universal method of calculation of the boundary layer. A
comparison of values obtained by this simplified method with
those of V.G. Sanoyan shown a difference which does not exceed
't~Q. A slight modification of the above equation to
- 2 JVT~'2 + VaUvero
r(x) + (6)
enables the profile to be calculated for the particular case of
flow past elongated bodies of revolution.
There is 1figure.
Card 2/3

Calculating the form of the inlet... S/147/62/000/001/005/015
E195/E135
ASSOCIATIOli:.Kafedra.aerogi(irodin.imiki, Kuybyshevskiy
aviatsionnyy institut
(Department of Aerohydrodynamics, Kuybyshev
Aviation Institute)
SUBMITTED:' April 24, 1961
Ir
U
Fig.1
Card 3/3

S/61 59/000/008/012/016
D218YI)304
AUTHOR: Filippov, G. Val Candidate of Technical Sciences
TITLE: the influence of roughness on the divergence effect
SOURCE: Kuybyshev, Industriallnyy institut. Sbornik nauchnykh
trudov, no. 8, 195,39 Teplotekhnika; voprosy teorii ra-
scheta i proyektirovaniya, 145-149
TEXT: Thin is a continuation of previous work reported by this
author (Ref. 1: Zhurnal Tekhnicheakoy fiziki, AN SSSR, XXVIII.,
1958). The theory developed in Ref. 1 is used to show that
/ko = 1 + 3975 d
A 1
derived in Ref. 1 for smooth pipes can also be used for rough pipes.
There are 1 figure, 2 tables and 2 Soviet-bloc references*
Card 1/1
7-d-M 71,
Q

S/196/62/000/010/015/035
E073/E155
AUTHOR: Filillpov, G-V-'
TITLE: On applying the boundary layer theory to investigating
the development of laminar flows of an incompressible
fluid in a plane diffusor with straight line
generatrices
PERIODICAL: Referativnyy zhurnal, Elektrotekhnika i energetilca,
no.10, 1962, 2, abstract 10 G9. (Tr. Kuy~yshevsk.
av3.ats. in-t, no.-l~, 1961, 135-144)
TEXT: A method is proposed of calculating the flow parameters
on the inlet section of a PlELne diffuser which permits calculating
the characteristics of the boundary layer and cbnsequently
determining the losses in the diffusor. Allowance for the
influence of the pressure gradient on the speed profile in the
boundary layer should refine the calculation. Thus it is necessary
to determine the point of transition of -the laminary boundary
layer into a turbulent one. 6 references.
FAbstractor's note; Complete translation'
Card 1/1

L 18790-63 EPAW/EWT(l)/M AFFTC/ASD Pd-4,
ACCESSION NRt AR3oo6436 S/0124/63/000/008/BD44/BC43
SOURCE: RZh. MeMumlkag. Abs. 8B267
~AUTHORt' X~lentiyev. V. M j~4e Ve'
~TITLE: Study of gas. efflux from commimicating vessels
.CITED SOURCEt Tr. Kuyby*shovsk. aviats. in-t, vy*p. 15, eh. 1, 1962, 99.104
~TOPIC TAGS: gas efflux, gas flow, isothemal-flow, stationar7 flow
.TRANSLATIONs This paper analyzes the stationary isothermal ;Mow of gas from two
colimunicating reservoirs in the atmosphere through an aperture which is in one of
them '. The flow from one of the containers to the other is also achieved through
an aperture in the partition which separates the reservoirs. Four possible schemes
of dependence on the relation of the external pressure and the pressure In the
neighbors - corresponding to four combinitions of the critical and pre critical pres-,i
sure Iftlls at the apertures. Each speoific process of efflux consists of several
phases corresponding to the indicated !system; the number of phases and the order of
their occurrenee depends on the parameters of the problem and the initdzl cofidi-
tions. 'On the -basis of known gas-dynanic formulas for each system a closed system
Card 112.
0M

L18?go-63.
ACCESSION XRt AR3006436 0
;of Zifferential equations is formed.- 1br the case when both the pressure falls: are
less than critical, the system can be integrated, only numerioallyl for the remain-
ing three cases, the solution is obtained in the form of a finite formula or as,
!integrals, which can be computed by the numerical method. The solution to the
derived system of equations makes it possible to obtain the dependence of the pros-
sure in the reservoirs on tinee The evDlution of the specific process can be cal-
;culated in stages.
To verify the method presented, an experimental study of the gas etflux oS air I
from commimicating neighboring eonta rs was conducted, with parameters; 43m
.vol=e, initial_pressure 1*036 kg/cm and temperature 298.50 in a medium with pres-
sure .436 kg/cm4~ with diameter of the ecternal aperture 4mm and the internal 2m.
~The pressure in the neighbors during eqimi intervals of time was measured In the
course of 15 min. In the efflux proceso only two phases occurred, since the cri.
cal pressure fall between the neighbors did not occur. The results of the experi-
mentaro plotted on the calculated cumis which are shown of the dependence of
prebmu-e in the containers on the time, corresponding to given initial conditiona
and parameters of the problem. 7he coincidence of the results of the calcastim
with the experimental data are good. 0. K. Kudin
DAT9 AOQ: 28Aug63 SUB COM AT. PH slims 00 "'T
Card 2/2

IVLENTIYEV, V.S.; FILIPPOV, G.V-
Studying the gas flow in coommicating vessels. Izv. vys. ucheb.
zav.; av. tekh. 6 no.2t8-10 163. -(KMA 160)
(Gas dynamics)
a-, ;!N-Pliyop

L 14666-66 EWr(l)/8Tr(m)/EPF(n)4 Jl)/IWW
AUG NM AT600308) SOURU
~Cwzl U014/ 000/015/0171/0176,
AUTHORS t lvlantiyev, Ve 3, F~~ov~ Of. V.
-Ihatit~-ute--(Ku-i*'shevukiy.-iviatsionnyy -instita~'~;--Jogh-
K!ijbnhev-Aviatioa t
'67n ]pj~olbl
8-cientific4achnicZ:- CoRrerence ous of the Mechanics of ]A�ALd Ctpd Gas -
(Estorvaya nauchno4ekhnicheskaya,, k.onferwataijapo- voproaut mekhaniki zhidlcosti i:A
gaza)--
v
,TlilE-. Pressure equalization in conneot(Kt containers
SOURCE: KuybyBhev. Aviatsionnyy Ustitut~ Trudyp no. 15; pt 2s 1963. Doklady
kust'ovoy nauchno-tokhnicheakoy konferentsli po voprosam makhaniki zhidkoati i
gaza (Reports of the.Joint saientific-technical conference on problems,of the
mechanics of liquid and gas), 171-176
TOPIC TAGSt adiabatic expwwionl,- thermodynamics., pressure distribution
ABSTRAM Th4 process of pressure equalization, between two adjacent voltuts is.
studied during a polytropio prooess
p A

RIBIN, Ivan Geargiyevich; FILIPPOV, I., red*; TBLEGINA, T., tekhn.red.
(Analysis of the economic operations of commercial enterpriseal
Analiz khosiaistvennoi doiatellnosti organizateii torgovli.
Koskva, Goefinizdat, 195!). 85 p. (MIRA 12:10)
(Russia-Commerce)

FILIPP07, I.; VITKOVA, N.
Now cooling syetems fo:r electric mcbines. RTO no-3:30 Mr '59-
(MMA 12:6)
(Blectric macbinery--Cooling)

FILIPPOV) Lp podpolkovnik, voyermyy rihturman pervogo klassa
Discipline on earth and in the air. Av. i kosm. 48
no.10:12-16 0 165. (MIRA 18:11)

:-:FILIPPOVI-- Iii--imbe-
Rapid assombly of a dressing plant. Stroitel no. 3:7-8 Mr 161.
(MBA 14:2)
(Marganets-4We dressipg--Equipment and supplies)

FIU;Tp% J.: ~_ _. ~ ~r:;,
PossibIlity Of Ming PailgriM Indicators. Nm.f3.ot 25 no.i:44 Ja 1165.
(MIRA 18:2)
1. Starahiy insh. saktcwa moreplayanlya Tgentrallnogo nauebno-
issled.olmtolvakogo instituta narokogo flota.

-9104--r-t- - - - ---
"Repair of a High Pressure Turbine Cylinder," Rab. energ., 2, No.4, 1952
0

22(3) SOV/174-58-5-34/37
AUTHOR: Filippov, I.A., Colonel
TITLE: The Development of Inventiveness in Artillery (Razvj-vat'
izobretatel'bkoye-tvorchestvo v artillerii)
PERIODICAL: Artilleriyskiy zhurnal, 1958, Nr 5, pp 54-55 M~3R)
ABSTRACT:. The author states that a number of inventions and
rationalizations have been made or sugFested by artillery-
men such as M.N. Belokur, G.F. Voroblyev, V.M.Kovalevs-
kiy and other regarding the modernization of PUO-3
(enabling to speed up the process of fixing and esti-
mating the number of artillery settings). N.N. Ivanov
and L.G. Turlushov suggested a device for fixing
meteorological and ballistic corrections. Lt Colonal
N.D. Mellchakov suggested a transformer of coordinates
for the stereoscopic rangefinder DS-0,9,Lieutenant
N.P. Ignato,v improved the loud-speaker used by the
battery covmander. It Colonel O.V. Sosyura,produced
Card 1/2
P

SOV/174-58-5-34/37
The Development of Inventiveness in jlrtillery
a new artillery logarithmic sliding rule. Major Ye.V.
Kuznetsov and SSt A,K. Bolodis made a monocular attach-
ment to a theodolite RT. A number of other improvements
of an organizational character was made to speed up and
improve fire control, such as a simplified angle com-
putor used during fire control. An exhibition of these
inventions was organised by the Service in 1957,
and the Journal described about 50 of them at about
that time.
Oard 2/2
2

--- - -- -----
HORTSOV O.A.; nITjPOVj_I.A.
Gradient appm,atus for measuring wlocity Ir. the 1cwar part
of the surface air layer above the sea. Ckeano2oglia I.; no.1-166-1-69
165. (MIRA 18:4)
1. Im-titut olceanologii AN SSSR.

GUREVICH, ~.L; ~mv Lk
Measurewfii~, af thI6
"mp
no. 22 -.37-AJ. 163 0
%
6, tu~-"6e mlm.~
'4r-~nt. Elektromila
(MIRA 17:1)
,Fly!

SAVELRYEV, V.P.; YOVALISKAYA, A.V.; BERUKOV., F.V.; GALKIN, Yu.F.- KROKHOTIN,
A.I.; SINEGUMIN, V.V.; EPSHTEYN, A.L.; TSIRKIN, Y.Z.; DIRUSMIA, N.S.;
G"9AREV, A.A.; KONTOROVICH, L.M.; KOROLEV, V.N.; USTIMMO, I.L.;
hUMAKOV, S.N.; POLUSHKIN) M.K.; LIBE, N.A.; IVANOV, N.P.; D'YACHENKO,
G.l.;~.FILIJ?POV,:1,,F,-;- 101UTORETSKIY, G.M.; VARTAWYAN, G.P.; RUSOV, Ye.Yh.;
BAMAN, UZ.; KOLONSKAYA, L.M.,- GORBAMMO, F.I.
Inventions. Energ. i ele'ktrotekh. prom, no,4.39 O-D 164,
(MiRA .180)

GUYERIGH, R.I., inzh.; FILIPPOV, I.F., inzh.; KRUTMETSKIY, G.M., inzh*
Anal7oiri of temperative distribution in turbogenerator rotors
with multijet cooling systems. Vest. elektroprom 34 no.6:5-8
je v 63, OURA 16:7)
(Turbogenerators)

IVANOV, N.P.; FILIPPOV I.F.
Methodology-for thermal -calculation of ele4dcal machines with
direct, cooling. Elektrichestvo no.1:17-21 Ja*163.
WMA 16 W
1, Lerdngradskiy filial Voesoyusn6go muchno-iseledovatellskogo
instituta elektromekhaniki,
(Electric rAchinery-Gooling)

FILIPPOV, losif Filippoyith;_ ZASLAVCKI--,', D.I., dots., retsenzent;
IvAfrOT='.P.-, ka-EEF. tekhxt. rauk, nauchr- red.; USSER,
A.S,,, kand. tekhn. nauk, red.; ZIFIVE, G.K., kand. teklui.
nauRp red.; ZARITSK.TY, Ya.V., red,
(Problems of the cooling of electrical machines] Vopros:,
okELazhdeniia elektricheakikki irfishin. Ynskva, Energiia,
196'+- 333 P. WIRA 18:1)

GUGELI, I.Ya,, Inzh.j PESOTSKAYA, K.V., inzh.; ROZOVSKAM, L.I,,, inzh.;
FILIPPOV I.F,,,inzh.
Study of the cooling system of enclosed DAZO motors with air-blow
cooling. Elektrotekhnika 35 no.9:20-22 S 164.
(MIRA 17:11)
Ng

Fnippov, I.F.
Method for designing a series of air coolers. Elektrosila no.19:
25--29 160. (Air conditioning) (MIRA, 15:2)
-4

GUREVICH, E.L, irnh.; FILIPPOV, I.F., inzh.
Device for measuring gas velocity in the channels of
electrical machines. Elektrotekhnika 36 no.8:5"0
Ag 1154, (KIRA 17.9)

FILIPF'Oli Inzh.
Method for ralculatlng the self -wintilation of the rotors of
elecr,rical machines. Elektrichestvo no.9:53-59 S 16-4-
(MTRA 17: 10)
1. Vsesoyuznyy nauchno-Issledovatel'skly institut elektromekhaniki,
Leningradskiy filial.

-05 C
-A
NO
~-~Wf- "Ric

MIR,` 311-'-173;

1PrOV, I.G. (Hooky&)
Solving a problem pertaining to vortex motion under the
swoface of a liquid In the case of Froude numbers close to
l.1Prikl.xat.i mekh. 24 no-3:478-490 My-Je'60. WMA 13:10)
(Fluid dynamics)

82497
S/040/60/024/04/12/023
AUTHOR: Filippo (110 scow C 111/ C 333
TITLf-:I,=i=mi=7Solitary Wave in Motion of a Vortex Below the Siiiface of
a Heavy Liquid'
PERIODIOAL: Prikladnaya matematika i mekhanika, 1960, Vo~. 24, No. 4,
pp. 714-717
TEXT: Me author considers the motion of a vortex with the,intensity
P below the surface of a heavy ideal liquid of the depth H.jIf c is,
the vortex velocity, then let
21
P ~ 0 > 1.
9H
Furthermore !,.et and ~ is assumed to characterize the
position.of depth of tNe vortex. By two successive conformal mappings
and by numerical integration of the arising integral equation the
author obtaijin the dependence of the magnitudes
2
Card 1/2

82497
S/040/16C)/024/04/12/023
C ill/ b'333
Limit Solitary Wave in Motion of a Vortex Below the Surface of a Heavy
Liquid
and C (coef:~icient of the lifting force) on and ~. For every value
T aA A thexe exists a -Mique value V (or-,,'c ) for-which a solitary
wave arises, whQre for V 4 VO (or c ~>oc ) ~'Iestruction of the wdve
takos place. A discussion of the solutioRs shows that a symmetric limit
wave is possible only for rV< 0 and small positive T" .
The author thanks N. N. Moiseyev for the guidance of the paper, and S.
A. SolovIyeva for the detailed calculation of the results. A. I.-. Ter-
Kr-ikorov is mentioned in the paper.
There are 3 :CiL,,ures, and 4 references' 3 Soviet and 1 American.
SUEIPNED: April 22, 1960
Card 2/2

FILIPB)V, I. G. Cand Phys-Nath Sai -- "On the movement of a vortex under aL
surface of heavy liquids" Moe, 1961 OXos Order of Lenin and Order of Labor
Red Berner State Univ im U. V. Lomonosov). (KL, 4-61, 185)
-49-

SHTWAII, I.D.,, inzh.; FILIPPOV, I.G., inzh.
Sinking inclined shafts in the Artem Mine. Shak-ht. stroi.
5 no.7:20-21 J1 161. (MIRA 15:6)
1. Krivorozhskiy filial Ukrainskogo muchno-issledovatel'skogo
instituta organizatsii i mekhanizatsii shakhtnogo stroitel'stva.
(Krivoy Rog Basin-SluLft sinking)

FILIPPOV I qt_,(M43skva)
Theo%7 of the difrraction of weak shock waves by contollre
of arbit-rarr shape. Prikle mate imekb, 27 no.1:75-44
Jh-F 163, (KM IN il)
M.- 5-VU
TO

FILIPPOV, I.G. (Mookva)
.......
Theory of linenr three-dimensional nQnstationary diffraction prob-
lems and some nonlinear problems, Prikl, mat. i mekh. 27 no.4:708-
72A. Jl-Ag 163. (11MA 16:9)
(Diffraction) (Shock waves)

FIL-',:PFOV, I.G. (Moskva)
Theory of the diffraction of plane elastic and electromagnetic waves*
Prikl& mat, i makhb 27 no.631026-1036 N-D '63., .(MIRA 17:1)
Omni

- - - - - -- ----- -
P
ACCESSICN NR: AP4027588 /0040/64/028/002/09916/OA
-V
AUTHOR: Filippovp Is 0. (Moscow)
TITLEt Theory of diffraction of cylindrical elastic and weak shook waves
SOURCE: Prikladnaya matematika i makhanika, ve 98# no* 2j 19640 296-304
TOPIC TAGS-. wave diffraction cylindrical waves elastic waves shock wave., two
dimensioaal problems nonstitionary-problemp second approximations wave propagation
ABST&WT: In two previous papers (K toorii difraktaii laby*kh udarny*kh voln
s
okolo ko- rov proizvollnoy fonkv*,. PI-M., 196 s t. 27s No, 1) and (K teorii.
atu 3
1, ch
3meyziyw prostranstvenny*kh nest4it6ionarny*kh zadach difraktaii i nakotory*yle
nclL-wyrXrrye zadachi. PMM., 1963j. i1p. 27y Noo 4) the author investigated and solved
nonstationary problems of diffraction of plane weak shock waves near contours of
arbitrary form. In this paper he generalizes his previous results to two-dimen-
sional nonstationary problems of diffraction of cylindrical weak shock and elastic
waves.. Ile gives general theorems which make it possible to study a o1 e b-
nd a Y pro
lems o4467 diffraction in a general famulatione He gives the solutions of mamr
roblems on diffraction in-quadratuires with consideration of the second approxLmaft ill.
p
&ard '1/2
Sri I EE~- I - -m a -1L
IVITTOMM"N

--YyVl~ -A ~4
/EWA (d)/-1-103 (k-) /IMA1 Pd-1
ACCE'SION NR: AP5011315 UR/0256/65/005/002/0230/M`5
533.6.011:51
AUTO Q: Filili#ov- I G
TTTU : Use of" the Volterra method in anIvIng certain problems on tite unstabir'
Itzed motion of an ideal compressible fluid
SOIJR,'E: Tnzhenerr-yy zhurnal, v. 5, n, -). 2, 1965, 230-235
TOPTO SAM- unstabiltzed fluid motion, cempressible ideal fluid, duotHriensional
prou em volution, blunt body, point~ad body problem, V,IlLerrd Metn,.~d
AP-RTIACT- no Vo~l"-rra #-p~roach is enuployed to solve linear problems an the un-
lizzd motion of an iieal compr~essible -'luid. The autl~or dealq SPf--'-ifiCa'.1y
itmen:ilonal probLems on the [enetratf -r~
1 .1 Jj-"r -,f idoal cr~vrr--qll~jo
Pthcr also applleq to wav- rerlpr':ior~ -rcn
-Ssior of a layer of fluid bv bluti- tlotll
1 )b I e-MG .Orig. art. has! 5 figur4~q anl 11 f - I
Card 1 (2
ASSO ;IATIMS None

1197~-66 (1)/E1V;)(MWW1(M MERFW-2
SOURCE COM UR/0208/65/005/006/l.W4/1031-.
ACC W AP6(X)OO14E'.'/A(h)/9'1;A(c)/ETC(m)_--_-,
IIJP W WWAM
AUTHOR.- Filippov., 1. 0. (Moscow)---
ORG: none
~TITLEt ',).n somil pioUlpli of the' diffraction-of weak shock waves ard-slastic waves
SOURGE:_ Zhurnal vychislitellney-matematiki. ffiatematicheskoy fisiki,, v.- 5P no.
1965, io?4-1m'.~
'TOPIC, TA, 318: shook waves shockwave diffraction~_cylirdric_-wave, Cauchy-problem,
-equati n- -a:diju ti
integral .0 9 8 c wave# wave-equation.,Volterra, equation,'iteration
wave diffraction
KBSTRAMI Several two-dimensional weak shoA problems are st~Ldied
*malytically over obstacl s ~- f various shapeWind geome ie
0 0 so The analysis is based
on the theorem that the diffraction problem i 's analogous to the Cauchy disolacement,
_Eroblem c tr the potential T in tho three-dimensional space (Xty The first problem
is the d ffractiAn of acoustic type waved frota a wedge (see Fig* 1)o The governing
Z;-, lit 5,;
Fig* 10
[LCqrd 1
517,92535,

OR
"'A I I

-6/
6 Ewr (,1.)/j _7A11
!Ah4iVQ!&7570 SOURCS~CODEt-"Uli/6198/66/002/002/0104/0109''
'AUT13011 t ow
Filipvov# L 0#' (Moso
tORG- none
TIT;.rFt On unateadrstate-problems:of a seml-infinite Aver of compreceible media
'SOURCE: Prikladnaya meManikag v. 2# no, 29 )9616, 104-109
1 TOP' .1.C, TAGS: compressiblo, flow, wave equation, unsteady flow, pressure distribution
'ourJace pressurep Cauchy'problem
asibldy aemi---~
JABSTRAMi The,problem-of a.plane pressure wave~penetrating a compre
i infinito layer of an Adeal fluid with no fA-0-tion was solved analytically.- The
TFMTT,t boEd-ed by a so]Td -wall and has a depth h. For times tit J - 1929 ... N9
0
ipreEisuro P (x1tt) is applied on the liquid surface f (x19t) so that the following
boundary and initial conditions hold,_
P,(x, E) d&-l .&t 0; j1(jt,1r)'