SCIENTIFIC ABSTRACT NIKOLSKIY, A. A. - NIKOLSKIY, A. P.

• Document Type: CREST
• Collection: Scientific Abstracts
• Document Number (FOIA) /ESDN (CREST): CIA-RDP86-00513R001137210010-5
• Release Decision: RIF
• Original Classification: S
• Document Page Count: 100
• Document Creation Date: January 3, 2017
• Document Release Date: August 1, 2000
• Sequence Number: 10
• Publication Date: December 31, 1967
• Content Type: SCIENTIFIC ABSTRACT

N-MI-ZlY A, A,
"InvastiMtion Of ~~;joratcd Vortex Flovs"
A Iaper presented ot the O,tb Internatioml Con,6ress of Applied
W-cl-onlAcs, Brimsels, 5-13, ScP 56

W/124-59-10-114&
Translation from% ReforativM thurnal, Mekhanike, 1959, No. 10, p. 61 (V$SR)
AUTHOR9 NIkol'skly, A. A.
TIZZ: Soso Exact Solutions of Thr**-Disonsional Gas Flow, Equations
PERIODICALt Sb. teor. rabot po "rodInamike. Moscow, Oborongic, 1957, PP. 27-33
The author search*& for the ol"s of thrto-dinjonglonal adlabatlc
gas nows, which are represented by the curve line I In the hodograph space.
The known Prandtl-Ptayer flows are obtained an a special case for the plane
I-eurve. He notes that the conxlder#d flows xay be used for solving the problem
of flow around unfoldUK wtngs with leading knife *Ues, specifically, conic
edges,ln a supersonic flow.
R. 0. Barantsev
Card 1/1

Translatinn fromt Referativnyy thurnal, MokhAnika, 1959, No. 10, Q (USSR)
AUTRORt A. k.
MAW t On the Adiabatic Gas Floj Class Represented In the Velocity
Hodograph Space by, Surface&
EMUODICALt Sb. toor. rabot po aerodInAmike. Moscow, Obcrovgix,. 195T, pp. 39-42
TMt The author studie3 the class of throo-diaensional steady adiabatic
gas flows, which are reprosent6d in the space of the velocity hodograph by, the
I-surfact desorlbed by the equation w a 0 (u, V), where u, v,. y are the
coordinates of the hodograph space. x, y, z are the coordinates of the flow
space, and 7 is the velocity potontial. The distr1trition funct Ion Is Introduced
in the shapet
X(u, v) - u x + v )r + w x
The equaticns of laminarity and continuity lead to equations or second order- for
the functions w (u, v) and (u, Y), It z - const-ant, first of' which Is quasillnear,
but the coefficients- of the second function are equal to the coorficients of' the,
first funation. Therefore, tht E-surfac* can. not bo6-arbitrary. A straight lina,
Card 1/2

SOV/124-59-10-L14W
Translation frost Roferativnyy shurnal, Nekhanika, 1959:, No. 10, pp. 60-61
(Usn)
AMOR; Nikol_lsk!&, A. A.
- ft-
TITUt On Bodies of Revolution Having an Internal Passage and External
Minim= Wave Impedance in Supersonic Flow I
PERIODICALt Sb. toor. rabot po aerodinamike. Koscow, Oboronglt, 1957, pp. 56-63
VEXT, Within tho frumork of the linear. theory', a, method Is. worked out
for determining the shape of a body off revolution having art Internal. passage and,
mLnlwAm wave impedance. The incident flow, the length, and thj~ radii at the endz-
of the tody of revolution are assumedto be giver, The wave impedance magnitude
of the body of revolution in not expressed by the pressure onto the body, which
should, necessitate w approximate solution, but by, & function on the reference
contour, which contains the characteristic., and closed by the required generatrix.
Suppressed passage of gas through the streazlined.body Is expr*ssod. also by-
functions on tl;-% reference contour. The arising varlatlon problem with. Iso-
porimetric condition is solved in explicit fom. A simple formula forthe wave
Card V/2

AUTHORs ;ikol'ALLZ,_A.A. (Moscow) 40-21-2-6/22
TITLEs On the Uplift and Induced Resistance of the Syet,~--i 7,ing-
Fuselage (0 nesushchikh evoyetvakh I lriduktivnom soprotiv-
lonit sistemy Irylo-fyuzelyazh)
PE1110DICALs Prikladneya Matematika I Uekhanika, 1957, 17ol 21, Fr 2
P1. 139-194
LBSTRAM Since for a con-ion flow of the wing and fua3lage under a cer-
tain angle of incidence the determination of the pressure
distribution on the surface of fuselage is difficult, the
anthor proposes a nethod which under certain asrunptiono al-
love to calculate the lift and the induced resistance from
the distritution of circulation along the wing spread (and
without the knowledge of the pressure distribution on the fu-
selage). It is assumed that the wing is a plane plate of ar-
bitrary form and that the fuselave is a body of r-volution
which can be replaced approximately by an Infinitely long cy-
linder. Further it is aasumed that the flow appears in an in-
compressible fluid for a small angle of flow and tinder a ne-
gligible friction. Lot the flow of the fugelage take place
without separation of flow. For the solution of the problem
Card 1/2

On the Uplift and Inducnd Resistance of the 3yetac lintr,- 40-21-2-4122
Fus,slage
the author makes the follo-rinG fundanzental assertions for
small aG also the intensity of the free whirl layer I- which
leaves the wing backwards is small and tends to ziro rithOt.
Therefore the elementary v7hirls of t for 4-#0 dist.-ibute
along the flow linoo of the axial-eymmetric flow -rhich appi!ars
at 41.,- 0. This fact permits to d*t*rmine the 4istribution of
the circulation of the whirl layer behinrl the body and the for-
ces acting on the whole system from the f;iven dint-ibtition of
circulation along the ning spread. There is I Soviet reference.
SUBMITTEN December 20,1956
AVAILABLEs Library of Congress
1. Tvaelages-Uft 2, distribatim
Wide of revolutim-Tban7
Card 2/2

AUM* KNS19=0 Ael~ 20-2-6/50
TMX1 The lassoonda fam of noWn of an Ulool fluld post a solid
(an investigatlon of d Is c on t Inuous vort1w] flow (0 Pvtoror
forme dvichaniya ideallnoy zhidkosti okolo obtqkqvwgo WA
(1n1*dovazdyootryvnykh vikhrevykh potakor)).
PERIODICALl Doklady Ak&do*UNa%k=,19579vol-116$Nr 29 PP-193-196(UsrR)
LBSTRACTs The author gives a somewhat more detailed reprecentation of
the lecture which was given in Brussels on September 12, 1956
on the occasion of the IX-th International Congress on
ApplI94 Mechanics.
ASSOCIATIONs Mechanical Institute, Acad.Sci. USSR (Inatitut dekha~iki
It N -33SR)
ZPLIBMITTEDi Novev.*:,er 9, 1956
AVAILABLEt Library ruf Congress
CARD 1/1

Inmimm, A*, A. (HOSCOV)
110A a" Flow In NZYMOUIC NOW"."
"On the Notion of Perfect FluJAs, and Gases for Which the Mommt of
Momentum about an Axis to ConstaiLt with Tim."
rnportepresented st the Fimt ALI-Union Corgreas on Theoretical and Applied
Mechanics, Moscow, 27 Jan - 3 Feb 1960.

71~1=--.011MA-1 rk, A.
030ralpmatca of HoUttme Fluids."
7-Ij-
"PO'ro*v PrOOOMWA &t tbamlatormtIonal Congrede of the Intornattocal Couwll
of AwromutIcal Sciamos, Zurlab, .9vitzerlAuA, IL-16 Sep 60

10 P!O~;cl T
I n
1 T7 t Tll,-
tjo(l ~'Ij jo
;n!2 if, I_X-lotll
u /Iirt o-p r, r I-: i:)
09 .T
D-017 V XC- -VI, Cl.
-17
U !'IL'
T
(T T_j
u 0.1 d, 4.1 c,-; 0'~Jn 'I or,
"17 T
JTi0t[ T n-

60111c pr .1 oblems of ihe hydr~,%dynamics ....
---- ---- --
b1z:i-hed, -thav in -the ,r, Otj zzu-d
th~. ratio of the ch.tr;_otf~ ri "-ni, ~,,f zh-
L)i
e i~A!;On pur ~-t,l
vc,
r
A:-1-14~.A A*~-D!11(--(.
-,Lic. s r. rn Z,-11 (s ho t --- rn-,
1-1pw of tile d"'11-1r.llic 0 ;*1 of a
-tvith tile F, ann e j 1,,~ Sj 0, f
t;,w
LAV :~f t)7,C,-
ti;e L'aturp ~4 1"'Lc
Lo Cho volucit), C, Ir n 04; Z
Z C, td f
i~; th,~ case st
ca-1 G-f r
4- U~ LL
re
t7lt,
lov" c.: rotating Vuid~- T.-c. *"-.c pa--r rnac-.- 1, 1 c
~~v t~-.c alathor .,~t tho 1', e
::-n ,I-.!ih.--1a-ngua;-c)
Card 2/2

S/124/62/000/004/004/030
D251/D301
A UTiiOR t Fikol'skij, A. A.
'AITLE., i:aglietoliydrodynamic motion with I frozen ' cirvulfir rat;-
1~etic lince
PERIODICkL: Referativnyy, zhurnal, M'ekhanika, no. 4, 1~62,. 1-2, n,ti-
stract 4B6 ~Inzhenernyy- zh., IIJ619 v. 1, no:. 1, 1.641-
175)
T EXT The axi-symmetric motion iv conjidered. of an, id,cal incom,
precuible liquid of infinite cunduutivity. The axial and
compon,ents of streas of the nagnetic field H are ausuried. equal to
Zero. It then follown from the equations of magnetic hydrodyn.-.nicu
tl~alu if at some initial inotant 11 = 'kr where ~, = conat -i-.d r is
t',ic d1utance from the axic of symmetry, then 11 = Ar Is preccrvel
evcryvi~el-o for all titc time of motion, and then the nyotom of Pqua-
tions of magnotic hydrodynamico coinciduc with the syeten of equa-
tiono for the motion of an ideal liquid in ordinary h.-i-drodytirimicu
Gard 1/ 2

NIFOLt!ZIT, A.A. (Moskva)
Hnwrtalic problems for r.&Lmetohydr,-4ynaxic notions of an Ideal
incompressible fluid with wfrr-n' circular naenetic lines. Inth,
shur. I no.2t4l-" 961. (KIRA 14:12)
1. Institut mekhaniki M SSSRe
(Kagnetohydrodynaitics)

9IIOLIaIYt %.At (Koekva)
"r&i'lieproblow for the Clow of an ideal incompressible fluid
tviated according to an arbitrary law. lnzh.z~ur. I no.2:149-1-52
,61. (KM 14:12)
(nuld dynaiales)

i
NIKDLJSKrT, A.A. (Koskv4)
Twee "tion of a hypemonic flow on eldmder bodies undw pg
radiation conditionx bt tho vicinity of tb* blufte", Insh-,shur,
1 uo.34045 161. (KML ISC2)
1, r"titut Mkbamw m am,
(Avrodyawdess Etr~oule)

5/020/61/137/003/006/OW
B1041214
AUTHOR: Nikol
TITLEt The syametric motion of an ideal liquid from a state in
which it rotatas like a solid body
PERIODICLLs Doklady- Akadsmii nauk SSSRO r. 137'o no. 5-t 1961, 537-540
TEXTI The author starts from. consideration of the systew of squatione
t 0
2*v*
p
+ 2ov, 0; 1- + 0.
W
,
desortbing the symmetric notion of an ideal incompressible liquid of'
denaYtjr q in cylindrical coordinates. Thi a; state of notion differs: only
littL* fron the rotation rith an angular velocity of a solid body, about
Card 1/6

Th*~eyunetria notion ... 31020~~,64 /I )T/0031006/0 301
B1041 214
the x-aria. Theatrean function 6a, tL*fyinC the Eq.
t ##N
is introduced Lm the, usual siamer, This equation possesses soliLtions of
ths fan
(dr3A*IkAT(X,11)j- 3L - r X, r - r It (0-
0
Here, IL (X,R) is, & real function, k & real or imaginary constant, and
ro & characteristic constant having the: dimension of' length., Proa this,
the author derive& the following system of equations which describes an
axially sysattrib potential motion of an incompressibleliquid with the
velocity potential Ib(Xj,R) and the str*&K function T(XjrR)*-
Card 2/

WOW
2Z56
-symmstria motion
51020161lt3,7100310061030.
The
X, (Ax. A (12)
rrp
I day+ a Or (13).
G M 0;
t Of n 67'
7F -r ax (14).
0.
jXt WEIR WR-)
L
By, satisfying the identitie,& 0 and 0 at t -we one, ottaine as,
)2, r
oolutiom of the ty 2~1 7 21 ir )(X R) *2k4-1t 6).
,pe (4): P' - Q ~" a t
Hexe, for imaginary k ik (k > 0) two principal cases are possible. The
following equations hold: For k > I
it, x for
X,
C&rd 5/6

The symstrio notion 5/020/6,1/15T(~05/!06/030
for 0