SCIENTIFIC ABSTRACT FR:KOSTYCHEV, G.I. TO:KOSTYANOVSKIY, R.C.
Document Type:
Collection:
Document Number (FOIA) /ESDN (CREST):
CIA-RDP86-00513R000825300047-6
Release Decision:
RIF
Original Classification:
U
Document Page Count:
99
Document Creation Date:
November 2, 2016
Sequence Number:
47
Case Number:
Publication Date:
December 31, 1967
Content Type:
SCIENTIFIC ABSTR
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CIA-RDP86-00513R000825300047-6.pdf | 7.43 MB |
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APPROVED FOR RELEASE. 06/23/11 CIA-RDP86-005138000825300047-6
APPROVED FOR RELEASE. 06/23/11 CIA-RDP86-005138000825300047-6
EIUTHORS: tiostychev, G�I., Polisovzzittov, V.I.
TITLE: Socne variational t~robl.er�r~s izz `as ct~-n~t~n_i.cs i'c~r
tttations other than steady-state
PEt~IODICr1L: Izvestiya vy,;shil.h ucliebnylch :~avedeni}r,
~\viatsionnaya telcllniica, zio.l, 1y62, 1.1-1~3
TEl'T: Many papers exist: �hich deal tivi.tli the dci:er;n~.natioz- c: f.
optitnu:a ;slues of tnissilc; dc~si`yzi par~:irneters, taut ~,rlixch ~:-r~~
applicable only to ste~aciy-state conch t;:i.on~,. Thc~ solut~c>izs it~ii,;
obtained do not apply to non-steady states tivhi.ch ch~.ir.n the ~~plane; the mapping;
funotion is t ivy i~
1 ~ 1 R~~~ 1 R~r -t 1
W j ~ ;~ ~ 1n ft--~, + ~ 1 ri ~ ~~ w t 9
where t~ is the path, a~i1 ~r the decieia,n of t1~e grid in the V~-plane and thel
parameter R is d.eterma.ned from ~. c~rt~j,. ra trl~,r~,{c;on~~~yrat equation. In tht.s
manner. In dz is determined. as a function of ~'by an integral of Schwarz.
Tn the papers of other authors on this gTZestion the analytic function
In dz was determined immediately in th~~~ infinitely connected domain of the
ti~-�plane; that caused large computing; difficul.tiesr since elliptic functions
were applied.
In an analogous manner the grid is i'ou~nci 4rri.~.r! consists of m congruent
profiles lying symmetrically around the coorclin.nte origin; here the
velocity distribution is given and. in the c�acr.dina.te origin there lies a
system consisting; of the vortex i :end thy; source ~..: In this case the
domain which corresponds to the .flo~v in the p_lanF~ 4'd 7_s mapped onto the ~
Card 2~3
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/G.d200v
~~~~~
Tz~ansTatian froma R~=fexativnyy ukrurr~.s.l .l~t.cern::r_I:i.~.ty ~~'~' J;,ilx g, p 69 (I~SSR)
AIITFiOR: Koatychev~G.I.
TITLE;: On the Construction of Grids Acca; rti.~z,~ tt~ ~ Glyn Ye ~r~~~xt y D ~.stribut ic~r
[Part af' the Dis~:e~�te,ti.an t"air:t~.ire~d iri 1y~~�i
1'ERIODICALs Tr,Kazanskdavis.t~~~in~tay1958y3~5~-3~y 1...1~
ABSTRACT: Let a grid with straight ayes c~ansi. t rf lnftn~.tely many F.n of ;~,.zc.h ~, g�rad from the vclocty
of flow given ae a func,tian of +,he pN,~:fi"le a.z~c: an the praf:.le, The
conditians oI' the problem per~it to dt�ter.rui.r.N~ -~13e ;~.b~olut.e value of the
deriva~;ive hf. the complex potential. PJ t3.s a f,,.r,ct on of the boundary point
of an :infinitely c:onnec:ted doms,in of th~~ ;t~~-,pl~;,n~-~ tivhi ch corz~esponds tea th:~
external reg%on of the sought grid., Thai men':i:~nec~ c]ama.in a~ the 'Nu~planE
is also a grid consisting of re~etilinear line:; s the pa~�a~r,eters of -this
grid are determined from the cond.~.ti.arra of the prc+b_i em~. In tha~s manliex t'rze
real part l.n ~z on the boundary Qfrhe :ini~ ni ~:e1y car~.noetecl dome.irr is
knowno For the determination r~~` ?r~ dtir' i;he auth.,~r maz1;~ the exfieriar of the
cl ~,
grid in thF; ~Lpl~,ne onto the exterinz� c,f ~!~r~c~-:n~tri^ un~,�. c:zrclps lying Il
Card 1~3
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On the Solution of a Variations,l Problem in Supersonic i~'lows
A and � are respectively the constant and the variable
multipliers of Lagrange , The lower indices denote
partial derivatives with respect to the pertinent
variables . 1~ith the use of tree first three of these
relations the fourth one can be transformed to read as
in Lq.lS. 'these four equations together with Eq.l1 will
enable us to detex~aine the five functions a{9 ~, ~-, ~ and
�. Lqu.15 is of the second order with respect -to ~s
hence the general solution of the system will contain
four arbitrary constants which can be determined by the
given magnitudes Y"a, ~ , Xo witri the help of Eq.l3 and
by the two boundary conditions at the free end (V~ T ~c)
which can be obtained from th� general form of the i`irst
Card 4/5
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SUV/147-5f3~-3-~I /1~
On the Solution of a Variational Problem in Supersonic flows
properties of the incident stream and of the angle of
the tangent to the shock wave in the. physical plane
(X, ~'), this angle given ~by Eq.7 . Taking into account the
standard relations throu;~h the shock wave as expressed b~-
the next threes equations and the relation `~, we can no~:~
obtain expressions as gi~u'en in Lq.B and g and these
finally lead 'to Eq.1Q. .A.long characteristics of the
second faudly there are 'two non-holonomic relations:
Equations 11 and 12. 't'hus we arrive at the following
variational problem: with the given parameters of the
incident stream (Eq.l) and the given magna.tude s ~a ;, ~
and g~ we have to determine tr-e functions ~((V~ ),
p (~V ), ~(~-) and ~ (~V) giving the minimum wave drag (Eq.4)
with the constant length Xo (Eq.10) and non-holonomic
relations of Eq.ll and 12. ~'or tha cases when the shock
is attached and there are no shocks or rarefaction waves
inside the triangle abc and on the assumption that the
speeds Tong tYie c~~.racteristi.c remain supersonic
throughout then, in accordance with the methods described
by the author (Ref .1) and Shmy~;levs' kiy (Ref .2) ~ four
Caz~. ~/5 x~c,l~at;ion:~ ~~x~ ob'~a~.i~o~~ r_-t~ ~;:i.vc~i~ k~~Y d'~c~.:l.ll ~ 1.r1 ~vi~~.c:l~
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~~ r
Cm the ;'olution of ~ Vax�is.tiona.l .k'z~o~s~.eui :in -~upersonic ~~']_ows
function . Let ~ (fir) be ~Ghe unl~zown :~'urzetion ~�~' --'
~a,ixi shock wave origina~~in~; at; a., then be~sua,~x~~ the
shock, the flow in the ~:rz~:~ng~.e ~,cd c~l~,nges o ~'~i~~h the
notation of Kef.l; thy; wave drag of tl~ze se~nen.t ab :is
given by Lq,3, where Z a.5 t;?1e contour based c~~:~, tae se ezat
ab, dssume now as the cozitour i, 'the curti~ acb (~~'i. ~ ~~
consisting of the shock: ~~,~,:. and the r
second family) be on j�iz~~.t in,~ a..- harac~~e ri;;t i c (~of th~~ .
the case when the fuzlcti.~~ns of t~~e ~gasgdvnaru.o~h?-~ also in
discontinuities in the z~;g~,or~ of in~;egration, hence ~.+;c~a~
can be integrated. clang ac ~,,y ~~aking the left lim:i,t of
the i'un~tions involved. o !l!rae ~t.~.te rz~.l a;lon ac bein
c g- _ g g
azzd o ~
tk~.t along be being ;;a:s s~iown izl ~~ef o:~ and ~)
~C~) ~~~~ sin ac ain (~.,.oc) � cos A dEV
I
The total wave drag o:~`C t;k~~ ~>ag~~i~::nt aU z~ g:LVer~ ley .~~~~zF
and the length of ~t,rzc .you. It body U.i re voluta_ozi i.s ~~er~
Card 2/5 by ~q.6o The function ~ (~) Ins,y be e . x�c;ssed. gi -
xx~ t e x m,, of
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_.,._
.~U`.THOR : I~4 Bt~Ch,~Y ~ ~.. G ~ I
~� ~....
'-~'-~`i'~~ Ua the ~olutlon of a Varia~l;~.on~~~, :i?.rob~.ezrr ~~n ~~tpersanic
I+~lows (K Re sheniyu oc~lo~y v~.riat si annoy zad.~.ch~.
sve rkhzvukovy.~1 t~: cheniy
r.~R10DlU.~L:ILVest;iya Vyssriikh UchE.bn~Tkh 7~avedeni~y=, .~vi at:~ionne,ya
Telshnika, 1858, i~r 3, AP ~GT7 (~SSSR)
~i~`z'N~CT: `.The author has already d~valt (Ref .l) with the problem
of the optimal shape of the nose of a body of
revolution (or a wing) giving a minimum wave drag in
a supersonic stream. '.There are ~ hovrever, cases when
axisynulletrical bodies are subjec~t;ed ~o a disturbed flow,
a og9 in a multi-stage ro~~j.~et w.~~ere tie disturbance is
caused by the main stage of the rocke--~ ~ Suppo, e it is
required to determine thE, an.a.pe of a body of revolution
having diameters 2~'a and ~.~'~ o~~r an a:~ial lezZ~~-~h ~U
(~'ig o ~. ~p:l.az~e C' , X) rE su:L~~~.Lz~~ in ~~he ri~~.n~.r~~,tl~ wat~~ drag in
a supersonic stream as dE3f fined by the parar~ete.rs of
Eqa 1, where f ~ (X, ~) are ~~ ~.ven ~.ontinuaus fun~,t ion, s
determined everywhere in t:he 'i'lov~r upstream stax~-~ing with
the characteristic (cif the fist faiui~.y) ad originating
Card l/5 at a (I+'ig ~ 2) 4 in the plaz.v~ (~ y ~) in u~~~ich ~ is the streams
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~osxYCx~rr, a, z,
Caln~le~ting the floa past ci~roular ~~aasdee of prefi'te~. 'Trudy ~.z
~~~rfl~ila)
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Corltrl_F~ut.:.c,:c to the px�ol~lenl ... X1.61/>'J~.l35
?llOf:ion, !`.~'; z;;,L`ci~, rc1C)rlf.itl~ltt~,, `; ,J tll,lt tllt~ !'t~LC"+~~i{.~; lttl ,if t71r
t'Tli't o!' f,lit? tlltlt.Lt~tl Stlolll.Ct i.1:i5Unl(' ,'1 F,{'.,1{.a.Ol1,1;")" ~Ft.t11F`, .~i 1'tlx'1~i1':LC?i3~71
Itlt?t:1OC} 1S IISCCh, C+;1;~1.Uy"121` Z.,rl!?;1";.111~~(? litt.l.l_'t;:L~"~ { :LLi.'S 7~I1:L"~ ].. (;~,it"']S to .9
comnlcl ec}u,.ltion :i.T1 wi~li.ctl t:i1e co~:f'1':i,r~ cnt: c?C file}~,t: tf�1-rl~; ciln ~~~
rn~lde �r.,er�o, till,i; 1c~.1~3itTG~; t:o ;j 1z F:t~. ,;llf'.['it: i_i'tlt e(~il.lt.i.c~n~, f.t,~ cl(~tc~rlu:ine~
then un!:zlowzl~. ~~ r,.1)~t:icul~lz' c.l~~t~ -� Ivllt~z) ~,i>t;?t~ n(' the r'llnctionM
].ntr odtlc(~d ,issl.tl,le si)c;~r.,:i.a1. fc):rlll;; -~ 1~.~,lcis t;o ~.tl(;,1.Q f. :i.f~~ci r.ozlcia~�ta.�n~.
i~ir.,zl]_~r, ecAua~:icrls ;re dF..riveci t'or ~;;lle shrl~c o�' thc~ lior(y whin the
1~rOZ:�;i C1O11C, C}llr'].T1C'; 1.11C '11O~.:1021 Lfi ~.1 L'ia.l'l_lilllli?l, Clnlt it l rO IthCll. 1: 71 t3 ~i~)!?f?(:~
of the body i.s CC)r]~tClilt;. `l'llt~t~'C' i.~7 1. (,i_~,Ilr(~.
:1SSGCI~'~'i,IOtiT: i~~lr;.lnsl.i.y ;lv:i.~tt~~i.orin~~~r :i.n.sti.knt:
i,1~t..f.,C'clr~l ilt,rOd1.31~1r1.l.k:i� (i~,zlan~ .1?'"t.11;],t)rl .L [1 .;~.ll.lt('
Dc'pax�trzent of Aex�adyrz~.lrna.cs )
SU';`1ITTisD: ;`.~~lrc}1 1]., 161
Card .'_/w'
~~`'
t~..
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t
i.. i,. ~(/'~;~
+~e
T'iL~. Corlt;r:~}~ut~;~rl to t1~e :7 1,
-T'C~ 1.er:i cif ti2E` tt I,i~_liil ~ .'cli~l' ~`.
i!t~illi:'S l.il lara~ t.;t~~:l ~l?'a'Cl f;tOi: t?I1
I'i~:.~.tt.-u_}:C \:i.,: :I�vrs;: .r.y.a ~";fssll:L?c}i i.lc}i~~lrraykla :~:EVEz~}=`r: t v.
^.v ,t;.;i.onn~~l}~;c tt~}cian.i?.,t, nc~.tl, 1~}t+} , ", , ;;'
~1~:.,,\.i: ~~+ilc' i1LIt',11O.1' COnti1C~cI'`~ ~1 tlUd}', t~llit'lt ~t{, .E ;?iii"} i.CiE',
r:lo~�ira`; i~a ~ t3~:~ jecto.ry cic�ined l,_y C,irt~sian coorct.i.n.,tes ~x,v} ,
T?lc~ "P :- m.C" ty1Jc t;clu,:ttl.oals o1' alt?ta.olt ;aa�c? a,~rc.t;t,i~rt ~in~rra lra
,rr;c:� ta~z.1_ ,lnd TZOrnr~11. forrir. ;llorlt; t:}le l~.lie cri fJ_i tlt, P i~ t;,
d_ Terence between the thrust anti tlae t:~ei.t}ii colrinanent plus t,ae
frontal resistalace to motion, tine lat t~~r tca�nl Mein; e~?~t�essed as
t.~e a ;z~e~zte of all the ele;:lental i esistances summed aver t:he i_+ra 3~�.
Normal to the line of flic;ht, P is flan c!i.f'.fer�crrtct~ hett.rrerl l.'nc~
1 a. i' t f
once, eti}~~ cussed as stn :Lnte~;r~al t,.i}ten over tlat~ l~oc~y
and tiaf,
~�:ei~ht COR1pO nc321t. The CroSS^~St'.Ct1~:111,:t1 5}att}tt' ,
OL' tt7e }Jody 1h
specified b}t tiro Cartesi an coordinates (~
r) , tdith t;lazs
introduction tlae Problellt nn~r con:~id~er~:cl ,
is t}lc~ ~ict~-~I'1I11.Ilat:1_c)Il of t},Fy
s}lal:re of tl~ae body, r = r(~ ), ,arid the taar~arir~~ tc~r~, def~ni.r~tg thca
Card 1/ 2
r .~~~,
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ONUFRlYEV, ~'imofey Grigor'yevich, dots; S};ATl~:L''. , }3ori.s P~ika7.ziyeva.ch,
dots., IVAt}'KU, 7`~mafay Yr~.kovlav~.r~a, ~.nzr~.; rlT;i~,t~,-:=,KA`~A, Lyt~Eiti7,r1
aer~oyovnrz, dot:.; SAItXCII'~"VA, iiintx F'at,rc~vna, r}at;~.; KI;S_'1"~A~'Pa'J,t
Sergey Petrovich,_. inzh. [deceased] ; YLGOtiUV,L.P.,dots., retse~azent;
2AY~Ti~`T~I{O,I .R, yr3ots. ,retsenzent; i3YALYt1I'1'SY.IY ,V .A. , inzh. ,rots�nrent;
CIiEEtKAS}ITN,N.A.,inzh.,retsena~ent; I~PdLh.,:}�To,inzh.,retsQnzen~t; PAUL'
V.P.,inzh.,red.; 2iL}`,I.,"PAYLVA, 7~.A.,~,nzh.,red~; t~'~DVF,DEVA, t~:.A.,
tekbn. red,
~hu~.ldinl;4~ in rallroud tx�~~~~c~I~r>i'tr~ta.c>ri] 'dr~rl3.lf~ n~: Ll~cy~.r~zr~c~uox�ozl~-
notn ixans~~orto. r'o;~kva, `Iran, rl,elritz~~a.rcl~.zt,, ~.~. (.'.~ IfG~.' I . (Z~iXI~~ 1~: t:~)
(ILa~lrouds---13~.i:i~.c1~.nE;s an~a st1�uctures)
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__-- _
---._ f ~
^ACC .NRi --.~~N6012199
' r ~.nd available training movies arc; not, ~-ls~d. T(lol~ t.U. ~
SOU~~CH. Tsentral'naya aerologiche3kaya ob:~c~rvatoriya. "~.'rudy, no. "(D, >~
-o ticheski e i ozonometrichepkiyo insledovaniya at~7a:~fezy (:~adYatiar~~�
Radiatsionno p Y
optical and ozonometrxc investigt~tions of thc~ atmoapherc), 4--57
TGP1C TAGS: radiosonde, actinometry, atmospheric eouriding, ntmospherl.c c;ial~d, I
at�ospheric radiation ~ ~
AB5 tRACa : (,h,:+nges in the long waive radiation of the earth's atmosphere dur:~ng a 7-- , 0 j
izr period are discussed on the basis of.' actinc,m~;trio radio;~onde drLt.~. c~'r,i.,:i_:.r~~::d ov~;'r F~
series of seven observ,~.txons at the 7.'sAO Aero).o~;ical I:r~atitut;e in Dol;;o~~,rudyy. 1~'c:~- ~~
I
seven radiosonde series are divided into three t,enera:t groups� 'h~ i~'~t `000`dec
. ~i`',,1c' second rr,ls do.:~_ ~:~51~ er so~.~.d
radiation field c;Ytanf;e:3 under cloudle.~s cundi~W:~on:z 1
cloud cUVt;T.'. ThB thl'ld 1'E~COrded GhtlT1~',',l;�j ~.ri t~lt3 ~�ViatlXOn~n A~`nUIIIbE?r,lv~({t}i`f;1~'~,~)lii'~G Fa.T'~ {T
conditions were changing rapidly during th� o}~Qer i
~;i.ven :~horv~.ng the changes in the affective xadxation field ir, the a.� ui, to an ~~
altitudo of 20 km. ~`rom thc~:~Q resulto it is conol.ud~.3d that ch,un~;es ~.n ~hC' lor,~; w~~vc~
i
Card i /2
u J ~ x____151 � c~� 1[
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I~ ACC NRi A"i'70O0567
i
f~ At1'i'1~Oi~.y ~ Ka;~tyanoy, C. N. ; Kurilo~va, Xu. V.
O~G: none'.
sou;:z~L co~~,: U~J~~r~~~~~/ooo/o~lo/co~i; oo~o~.
T:IT%,i;: On the radiation properties oi' cloudino:~r~
Si~U:3C:~: ~i'sentral'naya aerolo~icheskaya observatoriya. Trudy, no. 70, 1~ut,.
c?adiat;:>ionno-opticheskiye i oLOnomet:richetjkiye i.~t3ledovriniya rztmoufex^f ~~ucii.ationM
optical and o~.onometric inver~ti~;atioriu of thr_~ rstu~oop}~ar~,), 31-~gO
ioPIC Tt~G5: atmospheric cloud, atmospheric radiation, radioaor:de, at;,~oep;:c:r.ic
huraidi ty
ABS`iF~? CT: ~lhe effect of cloudiness on the a.on;, vrr~vc r,:id.~ati.on field of 4I `~
the frog aianosphere k~
t
CITED 54URCE: Tr. Tsentr. aerol._observ.~ ~'*p. 45,. 19dz, 73-~~
Td~~C TAGS; rad~t~.on orror, t~nperatur~s me~~r~morit~ tha~nal rosl,~tor rad~ca
sounding, atmospheric measurement, atmospher~.c temperature
TFtANSLATIONs The question of radiation erroa~s during the measureanent oj:' the
tFrnparature of the a,ir by ~~~s~tancesyp~;TRO~ which are used in rad~~o sound~.n~~;
of tho atmosphere. Formulas are introduc�d ~:or tho calculation of the Y~cat~.n~
the difference of temperature of the TR and tha sup^round3.ng air? for the TR's
. shielded and unshielded from the sun in the �ses when they are or~.ented hor~.7~on~
'tally and vort~.cally relative to the surface of the earth. The conditions dtu~ing
which xRs with co~rex~,ngs have the least heat'.ing are introduced. Recommi~ndations
are made with respect to decreasing the radiFition error of the transmitters used
ftx� ~.he mcasurement of tho ~,~,a;n~~era'tuc~ to tree Erse :~tn~osph~rc: ~~NCL~: t7C
i7ATE AG,~: 2$Aug6~ SUB CURE: A,3y PH ,-
Car d 1/1
APPROVED FOR RELEASE. 06/23/11 CIA-RDP86-005138000825300047-6
APPROVED FOR RELEASE. 06/23/11 CIA-RDP86-005138000825300047-6
APPROVED FOR RELEASE. 06/23/11 CIA-RDP86-005138000825300047-6
APPROVED FOR RELEASE. 06/23/11 CIA-RDP86-005138000825300047-6
APPROVED FOR RELEASE. 06/23/11 CIA-RDP86-005138000825300047-6
APPROVED FOR RELEASE. 06/23/11 CIA-RDP86-005138000825300047-6