SCIENTIFIC ABSTRACT SHATILOV, A.P. - SHATILOV, V.V.

• Document Type: CREST
• Collection: Scientific Abstracts
• Document Number (FOIA) /ESDN (CREST): CIA-RDP86-00513R001548710019-5
• Release Decision: RIF
• Original Classification: S
• Document Page Count: 100
• Document Creation Date: November 2, 2016
• Document Release Date: August 9, 2001
• Sequence Number: 19
• Publication Date: December 31, 1967
• Content Type: SCIENTIFIC ABSTRACT

SHATILOV) A. P.
Industrial testing of new drilling rigs for open-pit mining.
Gor. zhur. no.11:46-51 N 162. (MIRA 15:10)
1. Glavnyy spetsialist Gosudarstvennogo komiteta Soveta
Ministrov SSSR po avtomatizataii i mashinostrayeniyu.
(Boring machinery-Testing)

Ale),,:;Findr I ot ro Vic 11; CAM,057`111' SKI Y , I V;
LSve-rall !-,e za-, ion of in
the U.S.S.H.; material to aid lecturers 4a
mekhanizatsiia otk--.vtykh -o--nvkh ralbot., v SSSR; mate-
0 - '
~-ial v tomoshchl lektoru. .,oskva, Ob-vo "Zna-,.ie,"
RSFSR, 1963. 47 p. (~~JFLA 17:2P,)

SHATILOV, A.P., gornyy in2h.
Results of industrial tests of three-roller pin bits. Gor.
zhur. no.9:28-30 S 163. "MIRA 16-.10)

- . , ; , -,. j _ . . . ; ~ -, _ - -_ . _. ~' * , I" . . "I . ; 7 7 T T ' ' ~ - '. '.' " 1. ~' -~ !. -- . ; ~ *-, *. - 7' , - , , , , - . I "' n C~ C (~ "'., "
- . - - . . a . . . , I . .. - . . . - ~ I . k 'i - - i
"S'hoc'~-tute irvPstiJ-atIcn of the density behind the ref'Iected
r
S~Icc'. wave" .
rerort rresented at the 2nd All-Union con~Sress on rheoretical
and Vechanics3 ~,oscow, 20 Jan - 5 Felt 64.

L 20Q1Q-65 EVVT(1)/EWP(m EWG(v)/FCS (k )/EWA, (h)/M(I Pd' I/Pe-5/P.1-4 SSD(b)/
Alty-",'-r:r-~j~D/AFWL AEDC(a YB,"SD/ASD(f)-3/ASD(p)-j/AFETAR~/'OA I /C s -,4"' `~
OJM
0~gms
/T40480 710 0 0
ACCEbSION NR: ~i 2~ W IV/010T4O114
AV'THOR: Zavtsev,S.G Shatilov, A.P., Lazareva, Ye.V., Trukhanova, L.N., Averina,_-
A. _Yaichkov, M.K.
'."ITLE: Methods for measuring the density field of gas flow in a shock tube with the aid
of an interferometer
SOURCE: AN SSSR. Energeticheskiy institut.. Fizicheskaya gazodinamika I svoystva
gazov pri vy*sokikh temperaturakh (Physical gas dynamics and properties of gases at
high temperatures). Moscow, Izd-vo Nauka, 1964, 104-114
TOPIC TAGS: gas dynamics, gas density measurement, shock wave, shock tube, inter-
ferometry, nitrogen shock wave
ABSTRACT: The paper deals with techniques for interferometric studies of shock waveft
in a tube. The lengths of the high and low pressure tubes are 0. 9 and 3.4 m, respectively,
the internal cross section is 72 x 72 mm, and the side-walls of the end-section are made
of ~Lccurately (0. 2 band over the entire field) plane-parallel glass. A description of the
electronic details for recording, synchronization, etc. is then given. A Maolffi-Zehnder
interferom eter was us ed. Ille 'white' light source provided a light-pulse of A 11sec effective
length, by point and line-discharges of a capacitor charge to 10 kV. The scanning
Card 1/2

T59rap Fig. hIZO
L 20818-65
ACCESSION NR: 1411,10,18013
method allowed -sism; Mseus density measurement at a fixed plan with spatial
resolution of 1-1.5 sooo;i and time resolution of 2-3 psec. The electronic
recording system for framing,:~, photography is also described,
using an
-j-4 -3-"niade in the laboratory.of M. M. Bu lov, no that
41w. ts
the.high- speei'd__,~j41*1G1:M'f couldIbe recorded on, a fixedfilm. The sER-tof waids could be-
measured on a voAot~j.*L&:pe with an accuracy of less than 0. 1 of a band, and the maximum
and minimum WWWWTT_~ were measured with an MF-2 microphotometer. The method of
calibration is described and the total error in density determination is 'graiffied for
incident and reflected -folocks as a function of the Mach-number of the incident shock, in:
nitrogen with an initial 'tressure of 10 nim 11g and a temperature of 300K. Orig. art.
has: 11 f ig-ures and 6 :~viuations.
ASSOCIATION: 0rr47.M-'cheskiy Institut AN SSSR (Power Engineering In ute, AN SSSa)
SUBMITTED: 06Mar64 ENCL: 00 SUB CODE: ME
NO REF SOV: 006 OTHER: 002
Card 2/2
4~
0

L_~0820-65 EWP(m),/E','4-~(]--.)/EWT(1)/FCS(k)/EVIA(I)/ Pd-l/Pi-4/ BSD/SSD(b)/AFWL/
AM,(
a75~~D/ASM', )-3/A.SD(p)-3/AFETR/AFTC(a)/RAEM(a)/ESD(gs)AsD(t) mix
ACCESSION NR: AT4048014 S/0000/64/000/000/0115/0118,
AUTHOR: Zaytsev,-S.G Shatilov A-P.,-Lazareva, Ye. V,_ Trukhanova.
TITLE: Investigation of the interaction of a reflected shock with the boundary laye of
"J
flow behind an incident shock wave
SOURCE: AN SSSR. Energeticheskiy institut. Fizicheskaya gazodinamika isvoystva
gazov pri vy*sokikh temperaturakh (Physical gas dynamics and properties of gases at
high teml)eratures). Moscow, Izd-vo Nauka, 1964, 115-118
TOPIC TAGS: gas dynamics, shock wave, reflected shock wave, boundary lairer, inter-
ferometry, nitrogen shock wave
ABSTRACT, The paper gives the results of a study of the interaction of the front of a
91
reflected shock wave with the boundary layer of an oppositely directed flow, with the aid
of an interferometer and high-speed photography as described elsewhere in this same
volume. The experiments were carried out at Mach 3-7 and with initial pressures of 10
and 30 mm Hg in commercial nitrogen (about 0. 5% oxygen). The speed,was measured by
photographing a slitted-off part of the interference pattern on a film moving at 0. 117
mm/gsec, with an accuracy of 10% for incident and 15% for reflected waves. The density
Card 1/2

L 20820-65
ACCESSION NR: AT4048014
behind the front was also measured and found to be in agreement with calculated values.
The interference pattern showed that with Mach numbers up to 6, the perturbation
caused by interaction of the reflected shock with the boundary layer of the oppositely
directed flow was localized in a certain region adjoining the wall and moving with the
reflected shock. After passage of the reflectedwave, the gas again became homogeneous.
Orig. art. has: 4 figures.
ASSOCIATION: Energeticheskly institut AN SSSR (Power Engineering Institute,, AN SBSR)
SUBM1TTED: 06Mar64 ENCL: 00 SUB CODE: ME
NO REF SOV: 004 OTHER: 005
Card 2/2

L P0619-65 DqP(m)/EPF(c)/EPRAV1A (h)/E'IT(1)/EWT(m)/FCS(k)/E~IP(b)/EWP(t)/ Pd-1/
4 N'_
4 IJP(c)/SS6/AEDC(a)/SSI)(b)/AFWL/ASD(f )_3/ASD(p)_3/AFETR/ESD(qs)
JD/MILK
ACCESSION Nit: AT4048015 S/0000/64/000/060/0119/0126
AUTHOR: Zaytsev, S. G., Shatilov, A. P., Lazareva, Ye. V~ Trukhanova, L. N.
TITLE: Measurement of density behind a reflected shock wave in nitroge&
S6URCE- AN SSSR. Energeticheskiy institut. Fizicheskaya gazodinamika i Fivoystva
gazov pri vy*sokikh temperaturakh (Physical gas dynamics and properties of gases at
high teniperatures). Moscow, Izd-vo Nauka, 1964, 119-126
OPTC TAGS: gas dynamics, shock wave propagation, nitrogen shock wave, reflected
s..ock wave, gas density oscillatory relaxation
ABSTRACT: The paper is a continuation of previous work by the authors and deals with the
reflectior of a shock wave by the solid end of a shock-tube which contains industrial nigrogen
'(with about 0. 5% oxygen). Using fixed fflumination, the change in density with time was
determined by an interference method and recorded on film moving at 0. 117 nam/~ sec, both,
for tha iacident and reflected waves. The shocks propagated at Mach 3 to 6; the initial
pressures were 10 and 3 mm Hg, the maximum temperature in the reflected shock was
4000K and dissociation was 0. 2%. The equilibriUm and non-equilibrium densities for. a
s ection 5 2 mm from the end are graphed for Mach 2. 9, 3. 8 and 5. 6. The time to
Ca;.d 1/2

L 20819-65
ACCESSION NR: AT4048015
equilibrium density agrees with that of the oscillatory relaxation found by Blackman. The
density behind the reflected shock was also obtained by continuous scanning, ;at 3 mm
from the reflecting end of the tube where interaction with the boundary layer can be
neglected. At higher Mach numbers density. micreases with time; thus the density. becomes
greater than the calculated value and the divergence increases with time. The appendix
deals with equilibrium values of, thermodynamic parameters behind incident and reflected
shocks on the basis of mass, energy and momentum conservation and the equations of
state. The results for a shock in nitrogen at 300K and 10 mm Hg are tabulated, and
formulas are given for nonequillbrium values of thermodynamic parameters for incident
and reflected shock waves. Orig. art. hm 2 tables, 5 figures and 18 equations.
ASSOCIATION: Energeticheskiy institut AN SSSR (Power Engineering Institute, AN SSSR)
SUBMITTED: 06Mar64 ENCL: 00 SUB CODE: ME, TD
NO REF SOV: 008 OTHER: 000
Card 2/2

ACCESSION NRi AP40414736 S/0207/614/000/oc)4,10143/0149
AUTHORS: Zay-tsev) S. 0. (Moscow); Lazareva, Ye. V.(Moscow); Shatilovj A. F.
TITLE: Investigation of normal sh.,-k wave reflection in a shock tube
SOUME: ZhurrL&I prikladnoy molidianiki i tokNnicheskoy fiziki, no. 4, 1964,, 143-119
TOPIC TAGSz Nach number, argon, nitrogen, carbon dioxide, shock tube/ Mach Zender
interf erometer
ADSTRACT: The normal reflection of a shock wave from a solid wall was investigated
inside a 72 x 72 min shock tubo with It.5 mm low-pressure chamber length and 9 mm
high-pressure chamber length. Sliift in the interrerenco bands 6 S was determined
to within 0.1 band on a Mach-Zender interforometer. The absolute errors in densitar
for nitrogen, carbon dioxido, and argon gauos wore 0-308 X 10-5, 0-319 x lo-5, and
0.462 x 10-5 &,/cm3, respectively. First, tho state of tho gas behind the incident
shock wave was studied in N21 COV and argon gas for initial pressures of 10t 30,
and 100 mm, Hg respectively at 2,