SCIENTIFIC ABSTRACT PANCHENKOV, A. M. - PANCHENKOV, G. M.

• Document Type: CREST
• Collection: Scientific Abstracts
• Document Number (FOIA) /ESDN (CREST): CIA-RDP86-00513R001239010002-3
• Release Decision: RIF
• Original Classification: S
• Document Page Count: 100
• Document Creation Date: January 3, 2017
• Document Release Date: August 1, 2000
• Sequence Number: 2
• Publication Date: December 31, 1967
• Content Type: SCIENTIFIC ABSTRACT

S/021/62/000/002/005/010
Influence of shallows D299/D304
ASSOCIATION: Instytut hidrologiyi ta hidrotekhnilcy AN UkrRSR (In-
stitute of Hydrology and Hydraulic Engineering of
the AS UkrRSR)
PRESENTED: by Academician H. Ye. Pavlenko of the AS UkrRSR
SUBMITTED: July 31, 1961
Card 6/6

S/198/62/008/00-2/009/011
1)29~/D301
AUTHOR: Panchenkov, A, DT, (Kyyiv)
TITLE: Two-dimensional motion o.-L' a hydrofoil near the free
surface of a fluid
PERIODICAL; Pryk-ladna imelchanika, v. 8, no# 2# 1962t 200 - 213
TEXT: The motion of a submerged hydrofoil is considered. The theo-
ry of small waves is used, The problem is solved in the first appro-
ximation which is sufficient for practical calculations; therebyp
N.Ye. Kochin's function H(X) is introduced, the complex velocity
of the hydrofoil near the free surface being replaced bythe comp-
lex velocity of motion in an infinite stream* The function H is ex-
pressed by
H (k) (z) dz, (9)
CA
Thereupon, the expression for the hydrodynamic forces becomes:
Card 1/4

IOU6/002/009/011
S/198/62
Of D299/3)301
TV)o-di mensiOnal mot'o (V) +
iQ QT10F.- (10)
- 2a
P
.0
A
+ H (V -
t~,e air-
Kochin's f OrMula'
2ormula (10) differs substantiallY from h Of SubmersiOT3J a bo-
being independent of the dept Cting on
culv_tjon COD Completely determine the forces a e :~OD (Z)
ts one to a fluidt sinc
(10) -perM:L the free surface of finite stTeama
ay y1hich moves near body in the in
by the moti0l' Of the ,,istaqce are*.
d ' lift orce and the 'wave
pre determine he D (11)
The formUlas for t
_Q H (%) 12d), +QV IH(v-)v)V 7)~--r
P Qvor-- 2n
0
Q == QV I H (V)
(z) dz.
vIlle r e H V70
Card 2/4

3/196/62/008/002/009/011
Two-dimensional motion of a ... D299/D301 -
where the coefficients B, C, L can be readily determined. The follo-
wing particular cases are considered: A thin plate, a thin airfoil
-and Zhukovs1kiy's airfoil. The lift coefficient, calculated by the
ob-'U-a-.'4_ned formula, is in good agreement with the experimental results.
There are '3 figures and 7 reZerences: 6 Soviet-bloc and 1 non-So-
viet-bloc. T:ae reference to the English-language publication reads
as follows: T. Hishiama, Hydrodynamical investigation on submerged
hydrofoil, A.S.N.E., Journal, August, 1958.
.1
ASSOCIATION: Inslytut hidrolohiyi i hidroteklinilq AN URSR (Institu-
te of Hydrology and Hydraulic Engineering of the AS
UkrRSR)
SUB11ITTED: January 25P 1961
.,Card 4/4

r~,PA(b)/rylT(d)/FAS/t:,7(,n)/BDS/T-2--AFPPC/,~ D--P -4
ZACESSMIIT~N: JAII30DO/,61 5/0198/63/009/003/0331Y'0335
)V - -Wev) -
Kio~ XiOcb)ftenko~ -Aa I.-
IE' 'Establishing the optiumm relationships of quantities which characterize
the noticn, of a, ]&drofcil wing
I SOURCE; Prykladna makhanika, ir. 9, no. 3, 1963, 331-335
TOPICIAGS: hydrofoil-motion parameter, hydrotoil-wing lift,hydrofoil-wing
tb&
pt :-sngle W-rof6il enmwing
I.L4~~ -th-
S
tab near e-open:wtLter mwfa, ce.are discussed first.- The
tal dra
~g !)j~ 6' 10~rdoil andrelationships ariong drag components associated,witb
oPti='.lIft'-are considered in deriving formulas of the ovtimum
r ng,-t;;--=:Thew_for=la --::glv- nd
:v . Once: W
ep
_df _t
0 6i aL_ h- f submorsion,--aspeet-
PP_
-i~-ayd-dih6dral:tmglo-,of-:tt;o ving- dr -1-angle
--ra io~ 0 a
or aS a fUnction, of.these parameters is plotted in a diagram. A quadratic
equation- -in. -terms-or - nondimensional hydrodynamic and--constructional parameters of
4ihodral-wingv is derived. Dyneans -of. this -iqua-tlonp a propor
--t-
- ------------------

ACCIMSION ITR- AP402:3367 S/0198/64/01 0/002/ 0' 73/018 0
AUTHOR! PancUnkov A M, MR-nehm-kov, A. N.)(Kiev): St-Opanov, V, 0. ffitepanuv, V
TITLE:., A method for compui-ing the load distribution ovar the span of a hydrofoil
I, Y
Sr-K'rRf',E- Pry*kladna rnekharlika, v. 10, no. 2. A64, 173-180
TOPIC 7AGS: hydrod)mawrnicF, hvlirofell, ]()ad distribution, hvdrofoil loa-dirz, lift
AV lk
ti

L 69514-65
ACCESSION NR- A-P4023397
AMOCIATION: Inigty*tu,! mel~hwniky* AN T~RSRR of Mee+anlcr~ kN UT-Lilll
ST,93MTT*'."ED-. WDooUQ ENCIT, tin Cf--117 A
NO RIE"F SON: rpm,
C.?,d 2/2

PjUiCEENK011, A.N.
. I Approximate calculation of the lifting power of blado near
the free surface. PNTF no-4:67-68 N-D '60. (MIRA .14:7)
(Liff,(Aerodynamics))

[Panchenkov., -A.m.)
Practical met-hod of distpribution weights and water support in the move-
ment of vessels on under-water wings. Visti Inst. hidrol. i hidr.
URSR 19:51-61 1616 OIIRA 15:7)
(Planing hu.316) (Naval architecture)

FAITZENKOV, A. N. [Panchenkov, A.M. I
~2:-
Determining the coefficient, of lifting power of a slightly sulmerged
underwater wing. Visti Inst. hidrol. i hidr. All URSR 19:117-119 161.
(Planing hu3_113) - (MIRA 15:7)
P Y"

S/021/62/000/004/006/012
D299/D302
AUTHOR: Panchenkov, A.N.
TITIE: Recalculation of results of hydrofoil tests under
various conditions of motion
PERIODICAL: Akademiya nauk UkrRSR. Dopovidi, no. 49 1962p 452-455
TEXT: '."he formulas are given for recalculating results of tests
with hydrofoils of finite span to infinite span and from one span
to another. The working formula fo.- the lift coefficient of e. hydro-
foilp submerged to a depth hp with Pr v co (where b is
rb
the chord)t is IPO aco
CK (ao + (Lk - Aal).
~hk Voa- (I ~ 0
nx
where a0 - the angle of zero lift in an infinite stream; a k - the
angle of attack; Y a function (experimentally determined) which
0
Card 1/4

o06/012
/000/004/
/021 62
-D302
sular
(tile
of re BuLts Of surface on aw terms,
I Culat. fluellce 0 f t'" . ~ are 001-rectlo" ace.
TLeoa, - ae i aAa surf
0 omt the free
0 a,
taxes int je d'ae
f UlIctiol, to
t of 0 I:Lft 9119 the
.be zer imj)-
ooeff icien' it is 6 to (2)
Lai ti-, echange of 'resultsv &QI),
oceBsi'19 + Ch
_2k~~ d "ecal-
the pr a,.q
, n,~ (I + v I
I+ ~,% Vop '00 f OTV~Lila
foTmul felted
rJother -be
86 +
f rola 1+ ;~%~
aca (I + v1) 'be-
+ 10 (1- ilt oil tile lif t force
I+ % fluence Of prb zes actual 00a-
the in vhich characto e4ts eypeTi-
'Ment has 4 o 5 tyie t
cant vii-th ?,r'b many casest
I In
jrf ()JII3 xn6t_itute
colues 011 Of a -.Lng -of the AS U-kr
01: Iftoti
iditto
L-0 1411 2/41----

8/021/62/000/004/006/012
Recalculation of results of D299/D302
PRESENTED: by Academician H.Ye. Pavlenko, AS UkrRSR
SUBMITTED: August 15, 1961
Card 4/4

P)IICHENKOV? A., kand.fiz.-matem.nauk
Across the water on wings. Nauka i ziqttia 12 no.11:36-37 N
162. (MRA 16; 1)
(Hydroplane boats)

PAXCHM~'O.VA.N..[Panchenkov, A.M. ] (Kiyev)
Motion of a thin wing near the free mwface of a 2iquid,
Prykloaekh. 8 no,4:433-442 162. (MBA 15:9)
1, Institut gidrologii i gidrotelchnil-ki AN USSR.
(Hy&odynamics)
~~'T all-fP"

AC,
ES,
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expre,,j
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depth OD b fc,
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w"m
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nu

72._'6`ANM)~.W,T(d)/EWT(1)
NR' AT6016714 F14 F
Wr(M)1LVF(h)1T1EWP(1) W/DJ/GD
SOURCE CODE: UR/0000/65/000/000/0007/0020
AUTHOR:, PAn0h8nk.0v,-,j
jj
ORG,., -Institute of &dromeebanios AN UkrSS1 (11 nst.`4,ft3t gidromakhanik."L
AVUSSRr*w~
TITM, 0 -of- -a -il on the
-Lin or problems in the h1drgdyn -bydr6fo
boundary-surface,of fluids witb different densities
SOURCE.- AN UkrSSR. Gidrodinamika bollabik'n skorostey (High apeed
.11-1hydrody-namics),, no. 1,, Kiev,, Izd-vo Naukova dumka', 1965, 7-20
1" TOPIC TAGS: bydrodynarnic theory,, hydrofoil,, boundary layer tbeory
ABSTRACT: For a bearin~_Isurface witb a curvilinear axis* the potentials
0 and % (subscript 1 refers to the upper half space and subscript
2 t9 the lowl- half apace) are determined by the operators
card 1/2

A.CC NR;
-AT6004256 SOURCE CODE: TJ-'Z/0000/65/()00/000/0020/0032
AV11"HO'H: Tanchenkov,,.-A.1%. ,Oandidtite of physico-mathematical sciences)
ORG- 11 0-
93Ldrome:ohanlcal nsvitute of 'the AN UkrSSR (Institut gidr
melchaniki: AN,: UkrSSR)
-j
TITLE: A subwerged vane with small elongation
SOURCE,: jUl UrSSR. Issledovaniya po prikladnoy gidrodinamAke (Resea-.-ch
in applied hydrodynamics). Kiev, Izd-vo Naukova dumka, 1965, 20-32
G
TOPIC TA%37S: hydrodynamic theory, Froude number, Prandtl boundary layer
ABURACT; In-the-,oase of large and small Froude numberz, the theory
of. a vane with small -elongation has been-successfully generalized to
Include thelcase of a submerged vane. Rowever, difficulties are en-
countered in extending this theory to the case of arbilirary Froude
numbers., These di.Mculties are connected with determination, of 'the
assumptions 'Nihich must be introduced into the theory of a submerged
supporting surface at arbitrary Froude numbers. The present article
is a mathematioal.develoDment of the theory of a submerged vane wi-th
small elongation. As approximationr? for a vane w -ith ~ small -elongatian-t
the theory,taki?s the values-of-the--hydrom6dii~in--i-^.-al operators (the, po-
Vh 1,)ra
Itentials- 00--thi ocities,_tp and- of- e- acce - ~Ionsfe and the
Card L

_~a)/EPF(n) -21EWA(d) /FT('(m) WW
!L 9222-6& IT
'AGO NR,*.- AP60D0242 SQWX;E CODE: UR1019816510-,110101011510123-
0
iAUTHORS: Be3inskiy, V. G. (Kiev); Parchenkov, A. N. (Kiev)
~ORG: Instoitute of H&omechanics, AN UkrSSR (Institut gidromakhaniki.% A'.11 UkrSSR)
!TITLEi Motion of a vertical airfoil in liquid of finite depth
i SOURCE-. Prikladnaya mekhanika, v. 1. no. 10., 1965) 115-123
!TOPIC TAGS-t airfoil, singular integral lhtegral equation, hydrod~'namics,
i -
j incompressible flow
ABWEACT:, ~ The, method of acceleration potential is used to solve the linear
problem of a thin airfoil-moving in an incompressible fluid of fLnite depth H
with an arbitrary Froude number. The airfoil is immersed in the fluid vertically,
'at a ismn,', angle of attack cK and moves with 4% constant horizontal velocity VO.
1A-moving coordinate:system is adopted with the plane xy coinciding with the
undisturbed level of the fluid. The aeoiileratl.on potential is defined by
U.09.v:
the: 1-inear boundary, conditions at the free.liquid surface by

L 24287-bt, E"'Vk l)/EWP(m)/EPF(n)_2/E~?1A(d)/ET0 (za)-6 JKT/'i[W
J ACC Nk, atso.14221, (A0) SOURCE CODE: UR/010-0-/WdOP/004/0142/0143.,--
i_-,,rrJ;i.OF: P,.,jdien)cov4 A~ N.; Lukashenko, A. N.; ~h b
N. V.
r RG; -lone
-A
TITLE Scient-~fi C conference: on the hy drodynamics of a submerged foil
SOURCE: Prikladnaya mekhtLniia, 2, no. 4, 1966, 1h2-143
TOPIC TAGS: hydrodynamics 'flu d &jnamics,
low analysis, cavitation, cavity flow,
~Jb
olmdary layer flow
~AB,STRACT: A scientific conference on the aerohydrodynamics of a foil near a free
surface and a solid,surf' e f v
Sc was held at th iev. Institute o --& dromechani cs -of the
USSR A-cader 6__ or ____ f__ -45 Soviet
Selences from 2 1-30 Octob 10T, th 106 delegates rom
44istitutions participating. The folloifing scientific institutions were represented:
Cgr~tKAI_~~:~tnl~:afjc.:Research Institute im. Academician A. N. Kriov; Central Insti!MJg___
_2~_Aeroh~drodynamics; Institute of Hydrodynamics, Siberian Branch,, USSR Acadenrj of
-_,iTF_ _T _W___ --- ~ .
d S"'
racl IUe 0t ,,
s- -ter TrF a-
t
ke n. bij I
tion inee,,s; Central Scientific Research
fiovdsib~rsk and Gor1kiy Institutes of Water Trans tation Engin,e- --------
por ersi Kazan' and Kir--levi"
e nst L
A CTn'
State n i-u e
K
and Khar1koy Aviation Institute.._ Forty-one papers-were
ed which dealt wii~ ac+Ud__aerohydrocVna ~cDi;b_1_em'-s of high-speed objects, anong
Card 112

L ~:2
ACC NRi AP6014M
which -Pencliankov diiscuBsed problems of the unsteady motion
were the. following: A. N.
of-a foil at avariabledistance from a surface, and the hydrodynsmic boundary -4-alue
problem of a cavitating submerged foil. K. K. Fedyeyevskiy L)Xesented an approximate
-nonlinear theory-of :a-rectargular low-aspect-ratio foil-noving near a fluid surface
`a~ high Froude numbefs. V. 1. Rudomanov reported on takeoff (lift) and landing
&Jnanics 0:Ccral't utMzirg 9 urf ace ef fect. V - M, . Ivchanko reported on unsteac~r
,,(se+
hydrodynamic problems of supp..rcavitating bodies and them use - of elect:,,onic digital
computers in ropellerAesigni' G. A. Ryazanovis with electric flow simu-
P I - - _paper dealt
bion around'.:,foils of infinite span, and magnetic flow simulation around foils of
finite span. on the use of a magnetic simulation method
for estimating'.the effect of blade thicknesn in the desipp of a propeller with a
given blade -pressure differential. V. A. Kas'Yanov and 0. N. B_oy2Lskiy reported on
investipatlo--',A made on electrohydrodynamic flows and on boundary-layer control along
a foil profile. .. Ye. D. *Udartsev reviewed inethods fox- the laminarization
of the boundairy iayer of Mc Svdrodyramic flows. Yu. K. Biktimirov reported on
specific features in plotting the potential of velocities caused by a source moving
in a fluid. R.'B. Nudellman discussed bodies moving in EL multilayer fluid, and
V. T. Tokarev reported on aquantum-hydrodynamical analojW and its application in
hydrodynamics problems. In n final statement, it is mentioned that the conference
emphasized the importance and. urgency of problems in aerohydrodjnamics of a foil near
-a~surface. -The lag of Soviet science in the study of supercavitating foils was also
:2
mentioned, arid a more intense study of three-dimensional cavitation problems was
recommended. It was agreed that the pixyxedin'gp of thin conference be published. (GE)
SUB CODE. -13~--Ofj --- 20-V--j'
Card AT.9. Pone Y1 6'.

NRt AM501.32-10 MDNOGRAPH U11
Panchenkovp Anatoliy Nikolayevich
amics
Hydrofoil Wr2~n ~Gidrodinamika podvodnogo kryla) Kiov, Naukova dumka,
1965. 551 P. illus., biblio. 1p000 copies printed# (At head of title-, Akade
nauk Ukrainskoy SSR. Institut gidrodinamiki),
TOPIC TAGSs hydrodynamic theorys hydrofoil, motion mechanical unsteady flov,
dimensional flowf liquid flowp fluid mechanics, plane flow, fluid dynamicst
hydrodynamics
PURPOSE AND COVEME: This book presents the results of research on the theory of
hydrofoils, paying much attention to the mechanical and matnematical aspects and to
-the development of effective methods for solving the basic problems. The theory of
'-stes,4 notion of a hydrofoil of arbitrary- profile in plane parallel flow., the linea-
tized theory of a thin hydrofoil in plane mid in three-dimensional flow, and the
theory of a hydrofoil in unsteady flow are considered. Problems of interactlon of
h.Vdrofoils and of their motion near the interface of liquids of various density are
SUscussed in detail. The research results incorporated in Ch. VII were obtained by
~he author in cooperation with A. L lukhimenkop S. V. Kovallchuk, N.Y. Miodushevs
1. P. Tkaphenkes P. I. Ziwhukp aDd V. A. Stepanov. The author thanks N. A.
Ni1'chev0d_y_(C sponding Member AN Ukr5SR), F. F. Fillchakoy (Corres~nZig_XamFe_r
Card

I ACC NRs
M UkrSSR), 1. T. Yegorov (Dr. of Technical Sciences), M. YA. Alferly (Dr. of
T6-.hnical Sciences), M. M. Sidlyar (candidate of Physics and Mathematics), V. 1.
H6rkulov (Candidate of Physics and,M*athematics) A. V. Vasillyev (Candidate of Tech
Sk-lences), H. G. Starostin (Candidate of achnical Selene
14cal on)# V. 1. Putyate
Wmandiclate of Technical Salomon) p and D. V. Rode# A. G. Gubinp and V. H. Roman for
their discussions.
T*M CW CONTENTS Cabridged]t
Foreword -
Introduction - - 7
PAW 1. Theory of a hydrofoil in plane parallel flow
Ch* 1. Linearized theory of a thin hydrofoil in plans parallel flow 17
Ch. II. Theory of a hydrofoil ff:arbitrary profile in plans parallel flow - - 46
Ch. III. Theory of a hydrofoil in plans parallel flow of liquid of finite depth - -
Ch. IV. Interaction of hydrofoil in plane parallel flow - - 109
-Ch. V. Theory of hydrofoil in plans paral'iel unsteady flow - - 164
Ch. V1. Theory of a hydrofoil in plane parallel flow of liquids of various densities
. - - 196

ACC HReAM5013210
FiX Z, Theory of a hydrofoil three-dimensional flow
Ch. VII. Basic aspects of tho thoory of a hydrofoil of finito apan - - 229
Ch. VIII. Thoory of a hydrofoil in threo-dimensional flow of fluid of Infinite depth
-- 250
Ch. IX. Theory of a .)hydrofoil An thre"imensional flow of fluid or finite depth -
-- .386
Ch. X. Interaction nf hydrofoils in three-dimensional flow - - 410
Ch. XI. Theory of a kydrofoil in three-dimensional unsteady floij - - 433
Ch. XII. Fjotion of carrier systems near the interface between liquids of various
density - - 4%
[Bibliography] 540
SUB COM 20pl3l SUBM DAM 25Dac64/ WV REY t 17V OTH REF 1 060
Card, 3
13

?Alicllamv, m. M. PA76T68

PAVORENKOV, M.M.
Combination therapy of peptic ulcer with Gnaphalium and Fole-
-monium. Klin.med., Moskva no-3:92-93 Mr '50. (ODM 19:2)
1. Of the Hoopital 111herapautic Clinic (Director - Honored
Worker In Science Prof. D.A.Burmin), First Mosoow Order of
Lenin Medical Institute and of the Department of FharmacoloQ
(Head -- Honored Worker in Science Prof. V.V.Nikolayev) of thae
All-Union Institute of Medicinal and Aromatic Plants, Moscow.

PIVE V, M.M., dotsent
Professor D.A. Burmin, student of A.A. Ostroumov; anniversary
of his death. Terap.arkh-27 no.-):84-85 '55. (MLILA 8:9)
(BIOGiumigs,
Burmin. D.M.)

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U.- ftachrokov and Kh
10:1C, T.,
It M"11110i, gri, U. R. S, S,, Oajw xri. miajk~ mat,. V,,
r4ims, 111138, Mkii Anilivroiln- V. I- I,( I
IGM *41 1111441C Pf tile Oil 1. .4 "It Is, 1j,"Is Is-, Walk it, (I it fir.
111441 Ill, I'l"I" I lit I M hill, I'll% t.11111
silos is, I 411-14At its. (1 0 ~, fit- h l1p.t. 11.1l.ki A,hlia M
l1s.4, hiliv Wild I t lin'll I I'll. Allin-01 "Irk MI , I 1 01.1411%, of lowl fill--I ,if iwlsk, I
.444 1 ,, C 411,411t, Ill-virsk-441 flit- v of Ill, ,%Is 1,111 111will't W
01141-T st % -tsistil (it ~, tnill. %(,1V 1,14,~ lit It ., t
00 1 1 field of a gructator Wultraishott waves, 'r, . a 1111111olive lit flit diwIt'lice thc q Itim-440, the (it 141.4 to'
0 X wap covoled with running water to avold srxt-~_tfvor c;= which naphillAtrive wais titst Athirst alm, l1wirolotil 11111 Al A
tit the oil. The Increase In Pressture Inside the striNskilir loorf rate. Attila, of lOr' nal,1114,101or + 10% Unwell W
:0 J to ~pindlr oil decreal4rol I& imm. "leff. (it 9 httt undet '00
00 111111de rivorrm"ry 2-3 eVacustionst ditting a 10-hr. run ill v it Urvante prater than Isit
lltrvvnt clitinctilln (if lilt- dilorls;irgir, After a lit. flic attion I( th, 1;~Ilatv
lit. tun Afirt it nin its
be a i'llhe 4,114 food is lialliel n,hsr. Tile frillp. ctieff is( I'llyr '1451,111. ,It,
v 44 p1, dir solid filorlihir skills ItIctrawlt ft,tilelmhat sosillit, h(nit 'WI' is, 114'. Spilldic ,it lin,eVd -00
00 ild 11-01,11. lI,,Ih be tiflginal on(, fillic'.1k tindrit tile b1flil,llvv,4 tile di-hArer.
00 PolYffl(timl (414 weir Ittv list titivitd. ronvildii, The IxAtt vis*
pW#tb of rylindri and titaschine, oill; dristil"l, while that oil or*
opiodir oil slid nota cluinge. The atotnottle content tit flit
"4"t, 4,9 incTrassord by 1.4%, in usachine w3 it was pmc. 4*0
tiriilly rift"t. and In cylinder oil. It increloord by AfWMt
f 11.3%; *v"al orbrinft air mijig"Ied to sectioting fix goo
i I hor frort lotis In I he high frrqttrm-y dierhoirge. n. INd.- 00
:.t 1113~17(in Untilith, 1117).-Anintorwiplictim was nuidirrif solli
J!
ties
we*
;Il~ oig Qv M 0
is --- Is a a I W go 9 191 P_
op
U IF OF a It a r4 If x 1 x
0 s 0 %* *0 0 6 a 0 0 0 149 4 0 0 4 0 0 0 9 0 0 0 0
s 0 0 0 0 0 0 0 4111 0 0 0 0 41 0 0 0 0 0 e 0 0 a 0 e e 0 q 0 0 0 0 0 0

I ~z I t 3 1 1-9 9 m
A-A--L
g
00 w
00
00
0.
ille-$La
flux: 11111:11av.
0 0 6 S @Of* 0-4 0 a -v- 9 a a 0 0 0 9 0 9 a 9 0
lluumuls Ulf 19301 -2i- zin -)I a h v n P a it ij ji id il is v is it 'I, it U UC*
L-A- P1 w x T z -4 k 4 k-'- -A -J- A S A
lvt
wj -COE014t -1,11
$Vicki .1,
T
U it AV
0 It IV It .1 K
0 00 0 WO 00 0 0 0 0
00,9 0~0 0
6-10.0.0, 04 :
Us kledim betwen wtab in the pmeem of Jubd- -00
I K. V. K0111.8mant.,

ij 0. 637-440M.-Tive
. T.O. I.' S. JRW
J
polished metah lubri.
gowm ell* 6 kywered by cyclohn". myl -00
olek, valmitic Vind ftewic "S. Increasing
the qwwtity added (up to 24%) dtocre"n the Ptittil: -00
friction. while addrIs. of w-naphillylamine or cletyl ale.
Caulke a min. al k; at I I M" At a vanst. "Wwn- of the
A 1 4
4
1l
i
th
hi
h
*
1
h

.
e
rm"A
e
er
cr
. t
&sent 1.
g
addn. =jV1
mectsdins it) the nattarrof the invial isirclw'.
i%differmt
1
q
il
t (mm
ha
l
t
Th
(y
f
0
l t
rtru
. 4
11 04
cvt o
ul
(
n
e c
lWaft, etc.
)
their influmm on the interfacial tension brlwmn W %ad
kerutan
'90

goo
6*0

see

ale*

o(TALtURGICAL LIMATVAE CLAI$IFKATICII ~z
Ii71-5wt, a., Ill 90
I
re
a is a
00,
0 0 o
000 0 0 0
0 00 0 0 0 0 0 0 0 0 0 a 0 0

',A
09 ,1
a
00
eo
sea
06
4040
I t
a 6 800 0004 0 0 0 0 0 0 1 0 0 0 0 0
.4 v,- U 111 It LUA Al. V V - Do St 41 41 63 At (A
-2 I-A - ) - Is IL A--
ORWISM &1111 1`20401#1116 most
.00
-0
InweWpilon of 6* d1solocUk tome Is W smixtum
G.M.
PawhMV& juid 0. X. Daviyan. J. PLys. C". W. H.
H. It.) 13. d5l -V(IIkW).-The tatwat of IN ansle W di-
IwAu Ism ul the systems W011-twnseno (1) arAl 111M),-
K111sw6w 111) vat irs w lilt citswits. liatalkiwith

tuo-twhirlsustlimi tanklhis:4 toamal, *tN)% litolil -09
&nd YA1% PhNO, in I and H , , * 11w Vahme of tan Ag. X
10, ftw 1(1011 rlw f rom 00 , 0 to 91 .1 40% 410 thess
M
fall to 411 at ItK)% (h tim value W Wn At X
H1011) for
V
l
l
h
uroo
e
a
t
thur of rclauatko, r. cak-d. front the equation r - (Uv/-
Goo
5k T. as derived it= the Ilintelts viicosity equation, are
obtained trout the viticositics of the inixts. mid found to
frive values of the mol. radius half an "t as obtained front
L
l
i
d
d
d
l
an
iclor. data. The d
a
ne
ue to
he
smutpancy
s exp
"he rulallon of ibr tuals. conts, a Irmiltud txgar xtimip,
m00
P. 11. Rationalist we

800

Alf-ILA SIVALLMICAL 1,11111AUNIN CLAIJIFKATM
U A. AtIt mi A 6 a ew o 0 9 T-Iff-91 9
0 : 0 0 0 0 0 0 0 0 0 0 0 a 0 0 0 0 a 0 a 0 0 0 a * 0 0 0 0

flaw
0* Astler. KIWAin's farminh 9
*11M A Sbfi'q a-CMd" I3ILJYAjMb)qj6jJ
*0 relln"I" 4 thMP W 11bil "UMMICI
0 0 be valld &I Jkliffin
to%t it Is t1st
00 pro 103 Powl 44
tui M b" Vd. saw we W4 Vw 11
ftM 30" to 809, fi
goo
sea
**A
0
990
.0
43
0 0 0 9 0 0 6 a 0 0 a 0 a 0 0
11 a at
I,
eii vii
fldj seW tW
wahm all A it Am
It" a WSW.
few at "U.
&why* a' Oz
IBdWff=I ;,.V66,11Y '"ead WS and itil truipersh" dt.
hy&D- min
"adewil, ((,ubkin 1eirok
Init., hlowrnw). AW. Nauk S.-S.S.M., OWel. Tr1h.
Noah. Ing. p.
box Ifixt ZkWestri i Kolh7id. Rashwer (C-f- 10, VhCo'say a]
eawladed
--*--g aromatic COMP03.. w was
, -pars- of 1-141phenyla"adeca"
U31YI)IMMIKILIO. WW the examph of dib,il;i I.
diloydrodioctykatbratow abaft
1 TIME 133011FOCRIIII)IC 9 h "t necitawgir WSW the
the Iste"I chain. " UiAt have been concluiled
30 - Of dillrdrodirthYlanthrarew and dibydmdi.
!-tb--. 7U ir-temp. curve al d1hydrad
himthalmit is 00111whIlt Steeper than that of dl-
lortylanthraccae. vrhkh Sizan is at warbm wi
I-lisibutylpapilths3we sbm a
V 9 than 1.2.3.4-tetrahydro-1,4-dilso.
1, C0111trary to the red, 004 Inwensted
E-14~ydroaarbonx to be nwre v th" tin
mdW onximatic ampils. in varmaj. structural
46MAW so 1w by Twim Mutbms bave mly
vaWity. 7U wkwasky al hydrocarbons pla,
I OPPM. Wilit," Pwaty ady iftowparisainiare
to tMjx- 4 *gum slop" of the 94top. Curm.
1,40ids SOW eellin"J Mist.) 1. 139 1- 1! 1). (11 in
" It
IlachlitAil's l"flinalit V (vksuily) - Oit 1- 1.
r - Pp.vul.,ttirconst. wisliftqw%wrliotial tathrlw
roq.-r V.I.
ol the nx4..AAttn equal InO.JIr.M: thr Clum. r I- 3.&S, X
10-ITAI'ler'blAIIA, expre~--, the tent der lessIx..
Inasmuch as the formula can be der,vcd . I . nklint-tic
gas theory. It does not apply satiJactorily to lord.
liquktx or at temp. disiaril from the b.p.. ax inita;ra-'
I'Gils
between -60' and + IW. The
thcrinal variation If
this rrgion is much inurc prunouncT4 than pmlicled
inhe formula. (M Andrade formula, qP/s - Ae"'~
*here c Is a coast. involving the potential clicr". and the
other ImnulsWl- - Aei.rjk. whrrr k 6 the adislatir
runiprcsiblilly. lite f,winer III". not take into III
thmnal variathm tW the frripirnry of
give* twilrr awreaw, %till, (lot& (within 31;) tl=
9"M Call Do Cftlbttd 0 the Vahm of 9. 113
the saw. Vhboolty qw(M V)9/4 OW the
&k*wi"qMVSjvWt*bt&ddW".
tudem. 4=LdW wastim for the atom wall bcod toasts. of
:Vbeaphyan wexillarthellbsnp.dopeso
COMM; I bare III a Mrs. - far the ba groap. (3)
,I Pr*Vkm nP J. =MWW an Variation of V with pnmwm h
U 90 99y Me diKUX$ed
iianz Saone NEINN 0 AD a 2 a IF
0 0 0 0 41 0 0 0 0
k-0--oo 0:0 0-0 0 0 0 0 0 0 0 0 0 *
060
-00
-00
-00
got
goo
FOO
goo
goo
tso 0

A.
00 A
to -
00 Ai
00 A
0 t
Go&
'a 4, U U M U4 1, 0
JL_L_J__L
all MA 34if MY sips A) ad fsds~o
I' PDOCI IM No reoplatits '4DIS
F
4,661. INCRUSE IN V&SOOSITY OF OILS UNDIR IMAJENCZ OF A HIGH
FRF40INCT &MMMAGAVIC FIMD. Pam% To CA (SYMP. Visa.
p*9
0, Aced. 3ci. U.S~.S. 191.1, 1, 191-195;
L.Iquido and Uollold
J. last. Potrol. 19450 310 3204. Saku spUdlo. engine and
cylinder oils vero subjected to two note of oxPainsatts
(a) using frequencies of 12,ooo-im,wo Us. for 6 hre. Asa
the oils were placed In glass bottles, between theplates of a
condenser connected to the generator, end (b) using frequencies
of 1.6 x 107 Us. for 10 bra. and subjecting theoil to the affect
le,
of the Inductive discharge In the space boys the oil, in an
both typea of trestant Irvireased the viscosity
vessel.
of Us oils, the increase being more marked In the can* of (b);
VI wss little affected in eitber am&*. Results are expressed
gr&phially, including, in the ows of (a) currox relating
increase in viscosity to wave IsMO of the discharge.
NOW L
*0
0 10
.00
-00
-091
.001
roo
SOO
Woo
62~9 a I.,- so'~.V1 S01403 M4W Q"V 014 1814411CM11 914131 00V its
b - . . . .. . % F % - -1 -__V AAA so two M 911W91900599
U 12", 'D '410 900019011 walli Pia "t I xx
.,16 0 0 0 0 0
090000*0000000*0 000000
4

IS
Ar.
e I
o's
KK
t
flat) W
4548. PUMMILATION OF O-LS IN ELEMOMM HIGH FREOUENCY
D1SCHa,-E. Fa4.cbvjqy9 GH and Ulasov, IP (Trudy Moakov.
fiertyan. lust. in 3Y.0 4AWne, (Pro*. Gubkin Petrol. Inst.,
Moscow)$ 1946,
(4) 123-1271 abstr. in chem. abstr., 1950,
66114A121. Changes in the properties of an avaltion,
vol. 44,
oil (1) and the oil fraction of a cracking residue (b. 170-750
(11) caused by-an sle-tro4elass, high frequency diveharge
were studied
by the m;thod ured previously. Results of
experiments of 10,, 20# and 30 hours were admpared, Denoity,
molecular. weight and surface tension for the oil water
~nterfaca of both oils increased abd f.p. decreased with duration
of the discharge. Increase in )t per unit time was greater
for 1 than for U. burface tension for the air oil interface
remained constant. Aromatic content of I remained practically
conotunt but :~ncfesssd in 11. Percentage of unsaturated
hydroprbovairgoreased in I but temained unch*nged in 11.
CA
94TALU04VAL MUR41M CLAISWKATIO*
so
roe
real
roe
see
we 0
too
see
1., sek~.f. solo",) .11 G- CS4 G-1 ill
U it 4, .0 is T- V 171 An I a 'M 0 a W 1 9 IN 9 A 0
In a Pt a R tt a KW a 1 1X4
al () 0 a 0 9,40 009 06 Is 0 0 0 Is 0 0 91, 0 0 0 0 Is 0, 0
0.0 0,0 01i a 0 a 0 o o g o 0 0 0 -0 0 goe, :1: : 00 a 0 0 & 4, 0 0 0 0 0 0 a 0 0 0

0OW
09 0
00. it
00
0
31 a 33
- _ C_ __O! _1106M _991
9, . IL -S.-L -AL, --I AA ING M ILK A. L-A-.L,
09016fts m.s.
Tempmturo tirpood"C* of the Vlocosity.9 pure liquids
(314le 11111y" hjoirow). J. PAyi.
20. Hit-33(191(1)(In RuWatt):-
lAquids have a vi-cesity bemuse mats. from a slow kycr
temporazily ctxnbint with thoyA of a more W In AN
for a time move at an Intermediate ttpced.row. =r=
decream-s on an Increa-e of temp. becauw the mot. pairs
dimor. mwr trwilly then. This theory leads to nn rqua.
14mi conts. the V(Q. V of a mol., the Litent heat id valkwi-
ration. and the co6rdination number V of the liquid, litit
no arbitfitry emst. Reaumuble ho"tuntlitions 01 to the
values of rand -y afford an agreement between the rquatlmt
and lise expti. data. The riwation can be simplifitii un-
der cvrtAin conditions to Civ-_ the formuLus of Andrade
and lWhlnsktl. Ilikerm3n
A 1 o. I MULLWICAL 1,1111111AIMI CLAINFICATWO
34 is bi V a 0 a 41 a a it a
-0
^00
.00
-**6
I**
.00
Not
Q09
bee
uto, 6
too
U AV #A A I Z4 cm a a a I if 00
4M
OULO 0 0 0 40 0 0 0 0 0 0 0 r!e 0 0 0 * 0 : : : : :
0 102 idii~ : 0 :
0 1111040 to 0000 0 0 00 - - ___ __ - __ ____ 0-0:

A
W
ov~
I
palm SIVINk
-6 1- 18110#2 40 09V off
u is &v 10 LSI; a * I I I W 1 0 p
it 0 p so wafts Iran
010:::6:3866096000968
0.0 0 0 0 0 4, 9 0 0 :
llniv.. NIrr'(4nfl. J. MYS, (Vol.-
21;(IW)(i- R-60; c1. C.A. 40. W191 An-1 torrefftmo
atntf.-FMII the 11MUP. OWN. Of VbK%V4tT 'A biltAry MiXtI.
the 8v. entTory. of A*WM- cl 2 inoto. to n1rd. In the astur
manner &,I the nvwvrn, roagy ni unmixed fiquM, The
curvell I-MCA. CQUIJIL.. Mv Stfullitt when the ivwwn,
encron betwen ldentii--d and dillgrent mols. an similar
(v.x.. C#11c vxt CO.). hRv* a m1n. when the eurriv br.
twen two diffemt mots. is sma3. 49141 haVr a 111AX. in the
ON"ite caw. J..1Iikrr"Wn
zoo
r*
goo
.1 -99
MOO
300
wool
42.431 CM a- 4,
I ku 0 0 0 1 N It 1 .9 3 is v
*0060690 0 ease** 9
0:00
-k2-2-2-2-0 0 * 0 0 a 0 0 0 0 a 0

o*
00 It
go
0 *
jzj:
00
go
00
1 14 0 1 Q 11 11 11 14 11, it it 4 to x it 'W 8 8 A A I M U U IS 1A 9 A H 4 9- 0 U
Pit It ni~
Vimmity ~t Hqu14 mldwm G.
WOJ. Ulf. V. R'S.S. -3r; 41r~fflrjolay,-_R.
FeNd
comp
.
.
j*"fing abstralct.-A prcviuuJY dclivtd Formula 11w tim
dewatlem of viscoolty ci jjquj& an temp. *,A prmurt 0
can tw, uwA to cak. viscWties of mixts- it cOtmPOB(1'n9 40
vwUes for (Ise Iflist, wv -bitituttd And o. Is exprewd -
rl,l + earl. whetvrl. til Ond ft. on A" iht
+ 261
lrarlkm imud bond co"SY I- "Maskmetalt 1 1410 2.
alut As$ is tile InutuAl WhO ellerity,
m ol4ained fur the fatiolving Wilairf mixtIL: Cella'
allyl isoftleyalldr-
ca., C,110-11(oll, R. Wicb,-
piVkfim, McOH-watel.
0
CIO 0
400
as
adl
1& 0
too
it" 141OLI ~11 oat Amami
---Iwb law AV Ail, a (w a .1 w of 9 a a 3 a v 0
W_- I % ; 0 a 1161,61 111fl%1I "an 1411 11 1 M . I
All Is, 4) 0 0 4) 0 46,0 0 6 0 0 0 0 o a a ago*^* 0 a 0 0 0 0 0 0 0 0 0 0 0 : 0
': lie
~~ 0 0, 0 000 0 0 0 0 a 0 0 0 0
L7~ t/ 0 0 09 09 0 0 a

'L, L

0 i I ; i F ; T E III A II -V i A ItZ
OU I I nt:, 7
Ann "wisits c"ll

is
oe:
00 MOP. 10
.
'00
"00
we
00

DO
v6

go

two
too
VO 0
lb
""M Sol 041$l as O"T I"
184000 MV oil k&
It Gw Aa
q

0.0
00 ~o 0.6006 e40 0 0 00 0 0'0 SO tA
-00 000*00906*00600 90
OOo*e
0 *4
0- 0 0 0 4 0 0 0 0 0 0 0 0 0 0
*-*a- 0 G Ak. 4~.O 0.

oil - .... -w-

'0 0 'p
.7 64 OV 9 & 0 0 040's 0 so* 0 0 0 -0-0

0 0

Prmwo dopm4mce cd thi Thioety of liqui4a. X-U-
(('.ubkIn Petrokum 11int., Al""W). J.
9y
.,
~
:.
Phyl. ju.8-9
K
) 21
7,(,n R
.
.
.
q, CA, 40,601t". 41,229U.-Thcequat
vmijy is tested for meoll, ato!l. I -propanol, c^,htr. mild
' we*
RtBf UP to 12,000 Att". using Dridunan
s apti. Itata,
lm
Th
l vi
it
f 11
d
h
0 j
off
e
A
mmA
scos
n trAcc
to t
y o
e prroure
1
cEect on the intensity oi its intermol. form,
ova
X99

'too!

091"LW"AL LITERAIWE CL&UPICAT" W*q
flow WHIAT
*$Demo .0 ("v Got DILIVIO411 Olkill ON 04v ask
-

u IS AV
1 1 1 a I I a
SA I g ad 0 N 2 '1 V M I do Q 2 10 V
44 6
C' ft
: :
0 0 0 0
I
0 a 0 090 000 0 0 0 0 a 000000 0 9 0 0 6 0 0 SO a 0

PANCHENKOV, G. MI. PA BT37
USSR/Gasoline - Production
Catalysts, Fuel
Feb "9)~
7
"An Investigation of the Kinetics of the Disproportionate of Hydrogen in Gaso-
lines as Factors of the Composition of Aluminum Silicate Catalysts," K. V. Topchieva,
G. M. Panchenkovs 4 PP
IICR Acad Scill Vol LV-*, No 6
Study of the decrease in the content of unsaturated hydrocarbons due to the redis-
tribution of hydrogen in a mixture of hydrocarbons inthe presende of sulphuric acid,
a phenomenon also occurring in the presence of synthetic aluntinum silicates.
8T37

PANCHENKO M.
Panchenkov, G. M. "Kinetic cre-.zking of cumene over aluminosilicate catalYsts,"
vestnik Mosk. un-tas 1948, No. 11, p. 133-36
So: U-3566, 15 "larch 53, (Letopis 'Zhurnal Inykh Statey, ".. 13, 1949)

USSR/Chemietry - "See, ~qactlmx of
Cheimistry - rinetics
Kinstice of Gas Oxemloal Rewtione in a Current,w
G. H. Panchenkov, Petrole= Inst Imeni Aoadwiclan
2.
r1oscov, 7t pp
2hur FIz Mile Val XXII, No 2
Gives general methodL for setting up difftwential
equaticno for rapid reactions occurring In current,
of homogeneous as well as heteroganeou- - -*are, in
the kinetic field of their activity. MxaXAe::'&6' show.
the basis for the dIfferotntial equations for., reaotimi,
speeds and-their Integration, vith the lutact~,to deter
I I i;~6 . I ~.. . 1 0"
mine ~ the speed ~*=xtazt. , Submitted Mstl;V -7-
QalY results obtainea from 33&,CCI04) did n6i-iioree
with -the others. Submitted 1T Jun 194T.

PA 35/,49T91
ice
Liquids Viscosity
HMtheMtjcFj -Applied
"Me Problem of Ccmputing Absolute valuBs of
-Viscosity for Idquids," G. M. Pandhenkcv, 3 PP,(,4:y.a/
mu, No 6
~-Dok Ak Iffauk &SISR" Vol
es mathematicia theory, foxwulaSy and detemina
e.'v 6j df
t=te alu
tion of cone _g i0solut
Viscosity for liquids. COMPUtesthe absolute
values for carbon tetrachloride and bvazene$anII
the necessary sterie =ltiple. submitted by Acad
P. A. Rebinder, 30 00t 48.
35/49T91

so:
so
W
0 AS
00 t
of
T11
a the 'It 168.
01 J1. thm
0
0
0
.09
0
of
'o
0
;390
nee
Coe
so
use
ties
Use
too
OL L11110"UNS
OIL
-~_1161111, ~.
so
'Doe
00

Cakelolm oil obetilsate valoom of 69 oolmotmm* W
but" Mowm).,Tb'.':
d. C. A, 414. VINW. - 11 v
thfWvtkal it- tuoll TiChAitire heittem gwjli.
of a =4_61C Wilw4wly is'ptup-oll I -
A
,AVOP/ a - 7 with .4 -
,.W01RUI 1, r
)7 V40,/, -is tsp. &SIR). wbtiv p
Ul
slesnolty. rossabs. terap., Nss Avapolm's, soos,, It - aug. wt..
R - a" Cars".. 0 - mosol. vol.. a - bsood entm for the W41,
ill the liquids vow. ham the Internal looleat beat of vaporiu-
Jim in ims. Tbt novel featuff Of the for"lulm 14 Ow ill-
clw~ioa of a aterk factor. exp- Where AS 6 the ell.
tropy Ch"O on larroation to a bm4 in The fitiukt. FAtKv
sisol~ dam are borkinS for a dirv~ check of the fUMUIA. 9111
luftftl wevillevoikm U nooodr., .4 and ft arr deld. by rxl)ll.
vahosea har 9 at two irmpo.j or In thris culvd, fist the rrillir
troop. i4livival. llbm I am"Won"ll between 4-Ou'l,
and txptl. vahms llor thr=ux lu
ttlm: Its. Ni. 0~' CO.
Cis, Ifts. I.Kh, SuM. Coll&, Celts. C '14. and loWslue. RK
heptam. the Safttaint Is Owd Wwren =1 mad SQ'K.
m01. Comts. an allots C". 6; tht famula for tbKnquid'.
cited. llor aterk factor Varies brotovoten 0.4 (for Its) and
0.02 Jr. for CCI#, C&W, vothim ed m two.. ptuid Jos mol.
dhownsium Isamu from other mourtmoo. Mirbel BmvUrt

i I A I, 1e 11 11 14 1 it 17 PC I
A~ M At
8'. it ii J,
T
NPUBMAMOM I oil 041 moxe
rt4
fq$ I.De.
a
A

1832, CZACIltiam of Cumene an Alimminodlicate Catalymis
of Different Compositions, (in Russian.) K. %'. Topchleva mW
t
G. N1. l
a~, Dokladif Akadenill Nauk SSSH (Reports of
h
A
&
f S
f
U
R
t
e
cA
.tny o
ciences o
the
SS
), new ser., v. 74, Oil.

W 21, 1950, p. 1109- 1112.
,
( 71te above was Investigated at 400*C. using cafal ts tairli
10, 16, 30 50 72, and 1003 A1.0. tied go
84
.2
r0" 6;1N

00 0 ,
,
,
02
SiOs. Wc;u6 obtained an the basis of 4 Propmed tbeorctiml
f
l
l
l
d
l
b
h
-
unnu
ose
a correspon
Very c
ese o
tained experfinenta
y to t
)y. Data are tabulated Rod charted.
40 r
SIC
$ a .1 L A MITALLURZICAL LIMAIIIIII CLASSIFKAIION
flaw, I&- . . .......
--Sib U 11 AV PO IS 1;
*--oleo* 0_0 &.04 6A
,
-00
.00
.00
as
;3001
:00
tA 0
be*
AAA if 8WO N V'lWNDd3Q 20 v;G!
0 0 0 0 0 0 0 0 0 0 41 0 0 0 9 0 0 41
# 0 * 0 0 0 .0 0 0 0 0 0 0 0 SO A.

E N
Jotirn. or Tnet.
%I ITo. 33~
Yar. 1.951
723, Kinvues 01 rueneration of zlumlno-vulujs~ calalysts. 0. M.Panchonkov- and
;~,ililnt'nnov. Itrest. And. Nank S.R.S.R.,"Jidd. Tekh. Nnul-, l0ril, 1513 1.-
pUon anti dingi-nin nm gis-rn or Inhominry rquipint-vit usod for atinlying before-
gencous reArlion of oxidn of rat coke. CM pntlirles, Coaled with ovk* (npprox
o 6%). am suspended in reaction Who frum opting hnianco (Pervvltlvif:~'! x 10, g)s
a,.Trnp welght of granules was a x 10 g. Cat h heated In %!rrntn of Inortr to
ramovo volatilen and air Infroditred vdien test to altoldrd. Phlo III J)rt .
a
synthetic At-Bi cat imm shiclIM. Coking wait by 63.1
Smeking or ago nil (It. 0-8 3,
1.11P. 245'0. 00% volat 300"G. pitrall'Ittit 01-fin/a, nromAtIcs 91%lat 416, 0. J'ArS6
took showed abactico circoko migrallan an Cat ont(hea, Rat* of oxidn (its shown by lpim't
Iti. wt of Cott tICIC) IncrOmses, t"Itt, air flow, tip to litniting vnltto or letter. cliffotvocm~:
between oicirr"lo at votionit tonip IN less marked fic low air flow. Vp to,approx
470* C oxidn role, Is Men, and sliniltir rnr n11 ent, nbavo this tomp InAlvitintil Alfferctmem
appear. Difflerchre In oxidn rate mith rat rivirticio mine In rkicivet only nt, torop
>M*C. Most Icals worecarriod outivith hourlyalr-flo* inicial'306,000*V61 air/Vol
tat. At high invan (>520* C) reltilivo rate nt oxidii deettilms Wth Incionalhl; roke
.host cat hnce~ 61o;v oppi-ox 6400 C, Wootinan1widorlhon eff"MW " I
ros Its hit
diOCilOKKII %l0 t nh " M WIV11-
Moh eivotgy filoilotit of Ilia Wit) or M,0M MI/0%1, Ahovii itill-laiiij) 62A to"" n*
Limiting Wilhes or Wort initi ralto politchi, 14 *hIch i nh trom
kinetic to diMision m bt s61-Cm enter tor -11.bac
glort oucM 0

PANOW1110 G. 110
eoilsu"INOVA. K. VA;RAUJURWU&jj. _.~
SHInkT-",Ta. Ta. ,,,.Igktor khimichaskikh nauk, professor;
Polyu4riz&~Jop of oils in an elootzodeless high-frequenc)y discharge.
T=dy M Ao,IltZlO-220 151. (mIaA IO:.j)
. (P017wrixation) ,

MCMITKOV, 0. 1316
USSR/Chemistry - Petroleum 21 may 51
"Conversion of Hydrocarbons on Aluminum Silicate Catalysts of Varying Composition,n
N. V. Topchieva,, Sh. Battalova.. G. M. Panchenkovp Moscow State U JMnJ M. V.
Lomonosov
It Dok Ak Waxlk SSSR" Vol MVM- , No --.. pp 501-504
Al silicate has effect similar to that of acidic catalysts,(sulfuric acid, phosphoric
acid, H F90 B F31 AlG13) and dissociates under formation of H-ions. Its catalytic
effect is produced by compd Finilar in compn to montmorillonite: Kinetic investiga-
tions-on cracking of decalin, cetane, and gas oil over Al silicates of various
ccmpn,, but w-itb same sp surface, sbovied that effect is proportional to content of this
compd. in the catalyst#
186T13

t", Nt ~~Ls

o4
ZI

-FN
mom!.
-Ri
M

USSR)dhemistry - Viscosity of Hydro-. 21 Oct 51
carbons
"Viscosity and Molecular Structure) " G. X.
Panchenkov, Moscow Petroleum Inst imeai 1. M. Gubkin
I'Dok Ak Hauk SSSR11 Vol Unt, No 6, pp "-902
Studied the relationship between the viscosity of
liquids and their mol structure. Gives an exact
eq for this relationship as well as an approx one'.
The relationship in question was found to app'17
fairly vell to the homologous series of normal
?17T-9
straight-chain hydrocaYbons. Long ebains curl up
with a consequent reduction of viscosity. The eq
eapressing the temp de-pendencam of viscosity Is valid
for molten salts and metals as well as org liquids.
217T9

Ll-
USCH/Engineering - Fuel, Combustion Mar 52
"Kinetics of the Regeneration of Aluminosilicate
Catalysts: On the Mechanism of the Reaction of
Coke Oxidation on Aluminosilicate Catalysts," G. M.
Panchenko, N. V. Golovanov
"Iz Ak Nauk SSSR, Otdel Tekh Nauk" No 3, PP 384-394
Stating that technical literature gives no informa-
tian concerning coke oxidation on porous catalysts,
describes experiments for establishing possibility
for formation, under regeneration conditions, of
surface intermediate compounds of 0 with coke and
244T57
for studying formation kinetics of this complex.
Develops equation for oxidation rate of coals and
cokes in kinetic region under condition of constant
0 concentration along entire layer of catalyst.
Submitted by Acad A. V. Topabiyev, 30 Jan 51
244T57

USSR t"_,ngineeri~ \ Pup's, CoVllysis Jul 52
"Kinetics of tt4% ~Ag,,Per4tiOv OT Al';Millosi3-icatO
iqj~k~,',3tp Of Colw 011 Catalyst in Tubes
Catalysts: Ox,
WIth Variable COlacentration AlOrIg ~,he cat-
alyst Layer," 0, ~1,% VAachenicOv, 11. V. 403.ovailov
"Iz Ak Nauk, 4-0 Telth Hault" No I, PP 1031-1-036
CU
CM Develops metho,4 AA! 'ralc& tiVe 13eriod, withii,
which require4 ~ Vz3rtjn irl regerjerating gar, is at-
tained at giv" e~-,t:~OVL of reaQtor, . alla 0 cO4,, ill
regenerating "t 4.-t pfiiiite Moiaent from beg:Lnnii2g
of regeneratiq,,A Owe of Otati.OWY C06talyst
and isothermal V~ A:KttOnA. A3Ao Metood is deVeloVed'
for oalcg 0 diaV~~AAtipll -eaoog reactIon zone ror
case of counter4k?.~ zdtLI)II of Iregenerating gas aOd
catalyst for isotropy, condl-tioias. Submitted bY
Acad A. V. Topc)~kk V,
228T85

- --BATTALOVA-0 Sh., PANCHENKO. G. M., TOPCHIYEVA-,-K. V-.- ---
Cetane
Kinetics of cracking cetane with various aluminosilicate catalysts. Zhur.fiz.khim,,
16,, No. 69 1952.
M2nth List 9_f Russian Accessions, Library of Congress, November 1952. Unclassified.

PANGHENKOV, G. M.
Gases, Kinetic Theory Of
Calculation of rates of chemical reactions in flowing gases. Zhur. fiz. khim. 26,
No. 3, 1952.
9. 'Monthly List of Russian Accessions, Library of Congress, September -1953, Unclassified.
2

USSR/Cbemistry - Hydrocarbons, Cracking Jun 52
Procexs~ Catalysts
'Tinatics of the Cracking of Cetan on Alvminosili-
cate Catalysts of Various Composition," Sb. Batta-
lova, G.M. Panchenkov, K-V. Topchieva, Moscov State
jU imeni M. V. Lomonosov
"Zhur Fiz Ehim" Vol XXVI, IFO 6, PP 903-909
i The catalysts investigated bad an identical magni-
tu4e of the surface accessible to cetane.mols.
~Catalysts of the comPn 30% A-1203,TO% SiO2 and Al~O
~:50% Siop 3;
vhich are the most acidic, were found to,:
be. more effective than the others. The energy of.:
activation and the.compa of the, li&t fradtl6n of
itbe cata.-lyzate do not dependon the cAtilyiVS
a which proves that the active ~ centers are
of the s type. The results in cipestion. con'-'
firm the original. assuraption by the aut)4ors that
the catalytic activity of aluminosi-licate-c is
duti to the chem, properties of acidic hydroalu-
~minosilicates.

Diffusion
V. Obreimovia
Usine 1.
liquids. Dola. Al", SSSR
icients in
dif-usicn coeff
diffracti()n 1-,dcroriet~x in deterraninc-l"
. 3,
86,
Jan A CO 5 Ons) Ubrary of ConFress
List of RU
Decembe 1952. UNCIASS'Ff'~D-

C~3R
I-ANCITMOVP G.- -M,
Duto: iluic ~01 1952
I, uIll I c. I-Imononlyr, dil'Irulttalaralc~;O MI'll-rcuetcdcl is vo
Souae: Doklatly "Ji-mdvait Nallik PA:, rp.
NoLo: lrvucntod~ by thti mmuller of 4 110 Of tCtollr
A. V. Topohlyev cn Jitly 6 19 5

l'TZ'IET3011A, Te. Y.
TJ3SR (600)
Cracking Process
7. Kinetics of catalytic cracking of gasoil, Lokl. Ali SSSR, 87, No. 1, 1952.
The kinetics of cracking gas oil to gasoline with the aid
of a specially constructed apparatus. Two catalysts were used: (1) 5% A120j's
95% S1021 (2) 30% Al 203., 70% S102. The catalytic cracking of hydrocarbons n the
presence of an alumiFlosilicate catalyst can be assumed to be a first-order reaction.
Some of the starting materials have.a low adsorption capacity while some of the conden-
sation products have a high adsorption capacity. An equation is given for the calcn
of the rate constant, which describes the process for both cat-ilysts used.
Presented by Acad. A. V. Topchiyev 1.3 Sep 52. 252m
9. Monthly LA,~
t of P
mssian Aeceosiont3, Librai~y of Corignso, Fobruary, 1953. Unclassified.

--TA-245T9-
WSR/chemistry - Fuels, Propellents 11 Nov 52
"Catalytic Cracking as a Consecutive Chemical
Reaction," 0. M. Panchenkov and V. S. Tretlya-
kova, Moscow Petroleum Inst imeni T. M. Gubkina
"Dovc Ak Ilauk SSSR" Vol 87, No 2, pp 237-240
The reaction of catalytic cracking of hydro-
carbons is considered in the light of its kine-
ties as an irre-,~ersible consecutive first-order
reaction. A mathematical treatment of the sub-
ject ic given. Presented by Acad A. V. Top-
chiyev 13 Sep 52.
245T9

Vc. 7-

T -7 IV
----- -----

on a isli5lr4f['6~ Y t f gazioui
t~v rates

a current, G" 1 1,
chimical reaLtions proceeding in a get N

'C
A-
- Nyagiev
ins
46
59&-8(1i
cf
27
.
.
.
.
~
,
,
-47 -49, 2160d -P
32ffj~ 1718c Orochko CA. amhenkov
'
(Iefc;d,,;'lvib gm~;aIlml and
rigM hydraMatic type 0,1 treat- .
ment hl' b;oth hoir6fencous and butcrogeneous, stationary
ond nom;tat-Miary, reversi6le and nonreversibirt., chein. reac-
Jong in a Streaming gm.. F. H. Rhthmoknxi

Mat
Ad
fIr 0-
~g 1H
t7w!
up yi_sz~~;~5,~~,4,
AWN
R MAS RZ
MU
M R

PANCHENKOT. G.)(.-
"40.",t,#4.*
Kinetics of chain reactions. Uch.zap.Nosk.un. no-164:53-72 153.
-1
(Chemical reaction--Rate of) (KIRA 8:7)

G. i;.
EDT, k~w
Aftd. Nauk 5.5 NSR_.1 I
i I Py _M M S
d "d trans forms of decahydronaphthaleac over com.
alumosillcate catalyst was studied at 450-90'. Under the
same ccqdltkms the cis Isomer Is affected by the treatment
to a Ptlitt, extent than Is the tMA form, and an equil.
Mixt. Of the homers Sim an intermediate value. Tht,.
Ap mt rate of reaction A Is well represented by: k -
; MIJAM -log (I - X) - SL where Xt 6 the ISO, Of moles
entering the reaction zone, b the adjorption welf. ofdcca-
bYdrtmsPhthwJene,,U is the sum of Avduto of stokbiametric
wells, and adsorption cotfic. of producWWbich hinder the
reaction, I Is the length of the path, and z the amt. of con.
vertedmaterial. Thefollowingap arent k values am found:
-cis 480' -, 400' 0.03M, 470' 9,0354, 480' 0,04, 4901
0,0488; trutis 0.016. 0.0185, 0=15, 0,0274, 0.0=.
Activation energy for the cis form 13 14.700 W./ma'% that.
forthetransform(s22,200cal./mok. Theequil.mixt.has
the value of 18,400 cal./!nolc.. 0. M..Kosolspoff

I'l-f NC H !:-A(
-F-., 7! -77-- 1-1
-_7 77~ .71-21 7- -.7 -.7-
..........
NN
Ri

-hi- ly- hc -w)' V ~A -
USSR/Electronics - Ph(,-roeffect. Electron and Ion Emission, H-2
Abst Journal- Referat Zhur - F~Zjka, No 12, 1956, 35105
Author: Panchenkov) G. M., Akishin, P. A., Vw3illyev, N. N.
Institution: None
Title; On the Vnermionic 1hission of Silicate and Alumo-Silicate Ion Ex-
changers
Original
Perioclical: Dokl. AN SSSR, 1955, No 4, 571-574
Abstract: See Abstract 35104
Card 1/1

PA tic), e- ff
W~M/Electrtmico-. PhotoeffLict. E:Lectron and Ion Emission, H-2
ali Referat Zhur - Fizika, No 12, 1
Abet Journ 956) 35104
Authors Panchenkov.,
G. M., Akishin,, P. A., Vasillyev,, N. N.
instnullon t none
Title: On the Thermionic Emission of Silicate and Alumo-Silicate Ion Ex-
changers
Original'
Periodicals Vestn. Mosk. un.-ta.., 1955, No 8~, 3-15
Abstract: The authors remark that to obtain ions for the analysis of specimens
in the solid phase in-maos spectrometers one usually employs either
the ionization surfaces, or else thermionic emission from heated
salts. This work is devoted to experimental investigation of ion
exission of certain substances for the purpose of finding a suitable
emitter of ions for mass spectrometers. The objects studied were
combination products of- ions of alkali metals with alumo-silicates
of various ccmpositions. According to chemical and x-ray diffraction
data., the alkali ions do not enter into the composition of the
Card 1/2

XAMMV. A.A.; PAMMMXOV 1, G.M.
~ , -- " A ~,
- ~
Te"raturO and concent ' :~ nd
Of binary Sys ration dope an" Of the density and iac..,t.
tOMB of certain aromatic hydrocarbons. Zhur.fiz.khim.
29 no-7:1204-1220 JI 155. (KLRA 9:3) ,
1. *)skovskly COBudarstyannyY universitet ime Lomonosova.
(Aromatic compounds) Ili M*V*

--~~ -4 c
I I T., - /V /