SCIENTIFIC ABSTRACT GALKIN, V.S. - GALKINA, G.V.
Document Type:
Collection:
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
File:
Attachment | Size |
---|---|
CIA-RDP86-00513R000614120006-1.pdf | 3.73 MB |
Body:
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.