SCIENTIFIC ABSTRACT GALKIN, V.S. - GALKINA, G.V.

Document Type: 
Document Number (FOIA) /ESDN (CREST): 
CIA-RDP86-00513R000614120006-1
Release Decision: 
RIF
Original Classification: 
S
Document Page Count: 
100
Document Creation Date: 
November 2, 2016
Document Release Date: 
July 19, 2001
Sequence Number: 
6
Case Number: 
Publication Date: 
December 31, 1967
Content Type: 
SCIENTIFIC ABSTRACT
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PDF icon CIA-RDP86-00513R000614120006-1.pdf3.73 MB
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L 63007-61~ AC CESSION.-NR: AP5016271 P 10 + pVd -correct plane Couette flow qolutiou i Which tends to th i tl l oH- ii 6~ :0.. il L: 't~ 1 1: , ishowa that. them- above solutim is the:~ S~m of ~ -the' ~ kioo male~w w fl. ~he oontinUUM:SDlUtiOn given by the ITavier-Stokes: e(~mtiou~ 0 i jji;i a~l 111iAs i964i lati ms. ~IASSOGIATICNz none . ' SUMUTTED:.. EHOL i 100 P M IME. VT NO REF SM:~: OW C d 7 or , 2 2 7921-66 EWT(I~IW~z)IEWA(d 1ETC(z)1ZdA(1) WW'--- ACC NR:.AP5026695 SOURCE CODE-UR/0258/65/0051005/109 09581 54/ AUTHOR: (Mosc6w) ORG: None TITLE: Determination of the moments and forces acting on a rotating body in free;- molecular flow and in a light flux SOURCE: Inzhenernyy zhurnal- v. 5, no.,5 ~965,: 954 958 TOPIC TAGS: rotation, solid mechanics, fluid M(Mhgnic free =~o'lecular flow,-, light radiation- ABSTRACT: We designate by p and tau the normal and tangential components o ""the forces acting on an element of surface of the body, related to the veloCitj~ V2/2. The direction of tau is given by a unit vector 6f th ;ti gent to the, head P 0 an e, isurfaceof the body, t, directed so that V !jai 0-nx Xn y C40S 0- n Card 1/2 YJI)CM&A. 011. 8 7 7~ --L.10904-66, -e1tr(m)/r/E1VA(m)-2/EWA(h) IJP(c) r. NRi AP6002614 SOURCE CODE: uR/o258/65/005/006/1010/1020 va V. (Moscow) AUTHOR: Galkin, V. S. (Moscow); Gusev, V.- .(Moscow); Klirav ORG: none TITLE: Charac, 'teristics of a hypersonic, viscous gas flow patt bodies of simplest. shape.and their.aerodygamic characteristics SOURCE: -Inzhenernyy zhurnal, v. 5, no. 6, 1965. 1010-1020 TOPIC TAGS: hypersonic aerodynamics, aerodynamic characteristics., viscous flow,~ boundary layer, lift, drag coefficient, friction coefficient' ABSTRACT: This paper presents an- analysis of theoretical and experimental data~ obtained from a lar (19) of studies related to the,;characteristics of hXpersonic. iscous pRst slender sharp= i!nd lunt-n ,osed cones and their aerodynamic characteristics at various angles of attack in thermodynamically perfect gas flows. in section 1, hypersonic. viscous flows past heat-insulated and cooled (Tw.