SCIENTIFIC ABSTRACT PANEVA-KHOLEVICH, E. - PANFEROV, K. V.

• Document Type: CREST
• Collection: Scientific Abstracts
• Document Number (FOIA) /ESDN (CREST): CIA-RDP86-00513R001239010012-2
• Release Decision: RIF
• Original Classification: S
• Document Page Count: 100
• Document Creation Date: January 3, 2017
• Document Release Date: August 1, 2000
• Sequence Number: 12
• Publication Date: December 31, 1967
• Content Type: SCIENTIFIC ABSTRACT

KDXFORTI, B. -, PANNA-MIOLEVICH, I.; BUJMV, G.
Results of surgory of congenital hip dislocation using Zah-
radnicak's and Zabradnicek-Colonna'a methods., Khirargiiaj
Sofila 8 no.6:509-528 1955.
1. Institut za spetsializataiia i umvrohenstvnvane na lekarite
klinika po ortopediia i travmatologiia.
(HIP.,dislocations,
cown.,surg..,Zahradnicak's - Zahradnicek-Colonna's
technics)
(DISLOWIONS.
hip,congen.,surg., Zahradnicek's & Zahradnicak-Coloninals
technics)

PANVA-KHOLVICH, I., ml, asistent
Nalunited fractures of the extremities; causes and theraff.
Khirurgiia 7 no-3:154-171 1954.
1. Institut za. spetsializatelia i usuvurshenstvmvane na Iskari.
Klinika po ortopedlia i travrAtologiia. Zav, katedrata: prof,
B.Boichev.
(MGTURMS'
*extremlt'l-;,s. ms2united,;causes & ther.)
(XXMMITIESS fractures-,
causes tihor.)

PANLIVA-KHOUNICH, E.
Fracture of the radius in a typical case. Kbirurgiia, Sofia
8 no.4:340-347 1955.
1. Institut za spetsializataiia i usuvurshestvuvans na lekarite--
Sofiia Katedra po ortopedlia i travmatologiia. Zav.katedrata:
prof. B. Boichev.
(RADIM, fractures)
(FRACTURES,
radius)

13 i ~ LA5 0 f " Y ilrobie-rs ul"
A3'-~. JOUR. R2, B i 0 1 . , .-'-TC) - 12 19 58, No 5 6 222
B.
'the J-ijilikence of Vvcc~.n,;tAoT- on th-oz Titer of
pler!jent in Guinea
ORIG .PUB. Acta voterl.n., 1956, voi.6, Noa, 63-69
A F-3TRA C T Vacci:n-Ajon a~,a-,nst Salmonella enteriti0in Gerttier
in t4c. L,,uinea reduces the titer cov!nlement
(TC.) ddrin,~ c-ourtic i.,f 10 dvys: tl.e 1,)lwest 'Ic
on the Ath doy after the 2nd vaccinat-,011i
by the '110tii oav the IC ruturmi to normal

VEDERNIKOV M.; PRIZHKO M.; PANEVIN, D., starshiy master; KOBOZEV V.JO
.9 1 pre-
podavetell
Personnel for the giants of the chemical industry. Prof. tokh. obr.
21 no.1:8-9 Ja '64. (MIRA 17:3)
1. Direktor professionallno-tekhnicheskogo uchilishchs, No-53, Lu-
ganskaya, obl. (for Vedernikov)o 2. Zamestitell diroktora professio-
nallno-tekhnicheskogo uchilishcha, No-53p Luganskaya obl. (for Prizh-
ko).

25119
S/535/60/OOo/l19/Oo3/oc9
"W" 13 1 E194/E435
ALIT. H6714 Fctn~-%- it, f.?I, C-indidate of Techmical --cienec.;
T T T L7~" Fjuii HA'titi-lb-i-ticin in Oi.,~ nnray jet
r.r 7 ! I r-
p E R I D I C I a t's i t; nn Yy i ns t 1, t ti t , Trum 1 Y 119.
s y v t e p.1- Dv yhn d v, i 'r.
f ~') (.7 Ivipingini- Jet jiozzle.~ are dc: in -.)--ket eng1lie:E ond
.Lire Pre vi ous VIC, rl,,- c,-r, n -;zz I t- ~ii Vs i ts
'b' Th~ invinp~mrri-- two 4,~t:~ r-f n--,,i-
a 2- 1~' f! Ivy -,.7c d
b I f I U t -d --n 17 r C: f 1 6 t i c a I
C 0116 1 de r a t i or., Tile problem is simpilfied the prcc-,,~' is
symimetrical about ttit.- main r1iine %~hicb tf.c-- angle- of
-intfirt6ertior, of tk1c-- J~ts. Py r;pplyinr -rjuati:ir, fA
the .-A' energy) ania al6c equaticn~f -h~- CG?1S,-Y"-1at2-:n
of flov and c~f i,.omentum, an equation is dcriv'~-d f::~r -~hc fi *' :n
th, Omas :.~ a,: any p-sition, it J.5 fo'uncl -"A'.ar th., "ilm tbicki-It,!Z's
doe--t not d~ipend tzpor, the rale of flow of b'ut i4- a fun.-Ii,-'n -~.f
diatrieter and angle of )-mpact of the jets_ Test!~ were. --iadt~ t c.
-u-'y the flow and mixing of flt,,Jdc~ i1i i-ip* t ncizzLe-z, ar-A to
-1 11 - inglaig jc
C;'~- - d ) / r,

25119
5,516clof,,oli j-9/00/011-1~
A 9
ta,Iy the infliten.ce of the cnain injection parampt-.7-:: Two
cha.-.-ber-~ usea. '-n,.- at ~Jtrc!zrlb~,ric py-i-ssure itadc (if'
t, :.-I' F 4-1 A I -:~r- ItA c;;tr;- thi- ~Ath-r back-
could r-ange from. 40 t--: 180~', tbi-
I e-, d i arve I t~ r f r orno thin j.- 1f.,ngth f 12 to ~5110' mm,
C. the jt-.ts could be :!i-jp1acr-d late-ratlIN
III) tc Thr ter-1
'4e, f-- madr- with j&~!-, o' find . To th-~
f 1 u -~. c! i!. -i - f- -- - b u t j- on. i n t h z. a r r v y :ctAlecting head-ii wert -ziade up wi- h
a t-.-Y~bexr of r4c-set-ving, cell:~ each of collecting 10 -.1 -)f
d A Zfudy was A' the fluid 41-1-~tribut--on i-n the rt;ain
pl~lnf-, The amount collected at any position corresponds to th-~,
f Im thickness thera~ Chang-- iTi rate of flow. diameter and len,~- -i
icts not basically alter the ci:i-stribution law .Nhich sorretv:-~~t
A rormal ~au.-;E:ian df~itribution curve. A systematic
differenc=- i_- obser%ed it sm-aZl angles of impact betweea the tes--
results zi.nd the film t]-,tickness calculated by the recommended
formula and this i!~ perhaps due to the assuried aab-,ance :.f
tangential flow and may be due to surface tension, The foll:~wing
exp4-H.,ziental relationship is found for 0 4 a 60 (it ~s
Card 2/5

25119
S/535/60/000/119/003/009
Fluid distribution ... B194/E435
meaningless when
c,---)90*).
I + sin2 a - 2 sin a
+ s in2 a - 2 sin a cos (a4))
where h,,, is the actual relative film thickrie--s;
CX the angle between the- nozzle and the normal to the wain plane-,
a -0,32/3a - an experimental coeffacient.
Increising the angle of impact promote5 uniform fluid
disty.ibution in the main plane but increases the fIL-W backwards
from the main p2ans, The radial distribution of fluid is next
con-sicered. The th-iory of this case is more difficult because the
film formed by the impinging jet is destroyed by interaction with
the awbLent atnosp',,ere; this problem is considered in anotI7.er
paper of tiie autqo,, PP-85-101 Of this symposium. The ch!3racter
of the distribution depends mainly on the angle of impact,
increasing the .3jeetl and diameter of the jets -somewhat reduce,3 the
radial -,cattir of fluid, and the liquid distribution becomes more
Uniform. Aithough the curves have the general appearance of
Card 3/5

25119 S/535/6o/000/119/003/009
Fluid distribution ... E191;/E435
Gaussian distributions, application of the Gaussian laws does not
yield satisfactory results. The ratio of the two components at
different parts of the spray is considered. The ratio of the
components by weight is denoted k which is defined as the ratio
of the product of the specific gravity and amount of water
collected in the measuring glass to the corresponding product of
kerosene. Lines of equal values of k are parallel to the main
plane. Some spread occurs across the main plane probably because
jet flow conditions are not steady near to the point of impact.
Increasing the angle cf contact gives more uniform distribution of
components in the radial section and increasing the speed of flow
somewhat improves the mixing. The Influence of various injection
parameters on the distribution of liquids is considered. Speed
difference can be important if one jet speed is more than 20560 greater
than the other, one jet then penetrates the other and impairs
mixing. This does not occur if jets of the same speed are of
different diameters. If the jets are not coaxial (eccentric) the
main plane is rotated towards the central axis and if this
rotation is more than 300 mixing is impaired, Increasing the
length of the jets has the effect of increasing the eccentricity
Card 4/ 5

25,19
Fluid distribution S/535/60/000/119/003/009
E194/E435
and should# therefore, be restricted to less than five times the
diameter. Back pressure has little influence, Nozzles with
ILWO jets tend to throw back from the main plane, nozziss with
three jets in r)ne plan-, meeting at ti point do not do so, The
central jet prevents throw-back and is split into two, othr_r~iise
the distribution is generally similar to that for two jets and the
influence of angle speed and jet diameter on the fluid
di.qtribution of a three jet nozzle is much the same as for a two
jet. Thus, in many cases a three jet nozzle is better than a two
jet. A good difltributIon waq obtained with the two outer nozzles
delivering water and tht- c,~-ntral one kerosene at a speed 1.35 times
greater. The work de--~~-ribed was carried out In 1954-1955.
There are 5 figures nisd 4 rL-ferences; 2 Soviet and 2 non-Soviet.
The two references t3 Engli&h language publications read as follows:
Bond W., "The Proceedin,;.-, of' the Physical Society,r, 1.935, voi.47,
No.261; Kretschmar G., Wedaa H. Journal of the Optical Society
of America, 1953, Vol-43, No.6.
Card 5/5

25120
5/535/60/000/119/004/009
E194/E435
AUTHOR:
Panevin, I.G., Candidate of Technical Sciences
TITLE: The atomization of fluid by a nazzl,~~ with impinging jets
PERIODICAL. Mrct:cow, Aviatnionnyy instltut. Trudy, No.119, 1960.
Pabochiye protsissy v teplovykh dvAgatelInykh
uitanovkakh, PP.85-101
TEXT: Previous work on thin subject is briefly reviewed, there
appears to be no general agreement about the theory and the
problem of stability of a plani fluid layer moving in a gas
atmosphere is not fully solved. Previous wor1c dnes not
adequately con,4~-Jder short waves, which predominatoN in films in the
speed range covered, and does not give formulae for calculating the
optimum wavelength, In the author's preceeding paper ("Fluid
distribution in the spray from Impinging jet nozzles", PP~72-84 of
the present symposium) the flaw of a fluid film, formed by two
impinging jets is considered*. The present wark considers
breakdown of the film into drops, This is dont~ in three stages~
consideration of film stability; consid:!%ration of break up of film
.Lnto t1strings", consideration of break up of ".-3tringsl' into drops.
Card 1/7

The atomization o.L" fluid
25120 S/535/6o/ooo/n9/004/009
El94/E435
It is assumed that the liquid fIlm is flat and of unlimited extent
In the xz plane, ththt It moves progrt~seively and thnt the film and
surrounding gas are non-viscous and nicompressible. To assess
film stability, motion of a film of 12.quid in a statilt~nary gas
atmosphere acted upon by forces of surface tension and inertia is
considered. It is assumed that small oscillations of broad
frequency band occur at the intprfacc-., These oscillations may be
damped, may remain harmonic or may in-crease in amplitude and destroy
the film. Expres.-,ed mathematically, It is necessary to solve
simultaneously the fquations of main motion of th-2 film and of the
small oscillat3.on's of liquid in tha gas and to invcstigate the
stability of the sollation. Finally, the following expressions are
obtained-
=C(
(7)
where
Ot oz k) V 7
) ) ~C_ CA~,(iet-)]' (8)
Ck '(~V --5i I ~n. ~ ~a, -v
1. P t C, ( 4q. e~) V
Card 2/7 + I -L-rt -tkt V L)!'- (9)

25120
S/535/60/000/119/004/009
The ntomizritiou of fluid E394/E435
where h is half the film thickness; T is the period of
oscillation; o - 2W/T% k =- wavelengthi k = 21"/X;
V iz spi--Od Ot flow; Tb = P1.1,00 ii;; the relative density of the
gat,, whiOi 1.~; usuFt'Lly small, The stiffix c ci:jrresponds to
s)numetrical and the suffix H to asymmetrical oscillations,
It is shown that stability deptndi3 upon the value of 0, if
Inrmonic arid it P < 0 it Is Jitcrcaning. With both iymmetrical
and asyrtjli~-trj~al Osc"LlIations Ae may have
o the oscillation in dampeC if P - 0 oscil-lation is
Card 3/ 7

The ntomization of fluid
(XOPOH = 2.MPTV2 02(a)
1
25120 S/535/60/000/119/004/009
E194/9435
(13)
Formulae are given for tP2(A) arld qP2(a) which, howev-r, remain
constant for long waves at values cf Q2 --,1.3 and *~- A62~0
when the wavelength is over ten ti.-ies the half film thickn,Ic~s, these
values are approximately true down to wavelengths of times the
half film thickness, The boundary of stability for both types of
oscillation is given by the following
A !Z3 2W T o6)
0 P1V2
Break up of the film into strings !Lz then considered. Waves of
optimum wavelength are assumed to cause film break up, The
annular cards are assumed to be equal in width to the optimixin wave-
longth, Hence one can calculate the noction of the ring and tbe
film thickness at the place where the film breaks. At first, the
rings are not of circular section and so the usual methods of
assess.-ing stability are not suitablci and Blinov's method treast be
Card 4/7

25120
S/535/60/000/119/004/009
The atoi.-Azation of flaid E194/E435
used to atsess the ~5tability- Expressions are then derived fDr
the peri~A of oscillatior, c,f the ring and of drops whence an
expressi-~-i for the dr~.-,p -12arreter -As readily jr-rived by equotint; thr-
twO tLtre~ ("I) giving
) / ~ ~-Th 0-19)
dk
The experi-,.ental work wa.5 ca~rried out on the 2!quipmen-i as
that used for the work lesc-ibed in the pre--ri:~u,.; orticle (rP,72-8'*
Same synpo6ium), The influpnce of the main linjection parameters
was studied on water using nr)zzle diameters of I to 2 mm, nngles
of impingement of 40 to 1600 and nozzle prossure dLops of I to
15 atm. Drops were trapped on a smoked plate -.f-7th 1- soot layer
greater than 1.5 time6 the drop diameter, Arringements wcrP made
to expo5e these sheets for v,-ry short times. Thsy -wt~re examined
microscopically, Sparli photography of the bpr.--y wa-~ also used.
The phot!--graphs showed that break up could be duE to both
symmetrical acid asymmetrical oscillattons, Thc wavclength is
Card 5/7

25120 S/535/6o/ooo,'l1q/oo4/ooq
The atomizatic-n of fluid E194/E435
generally in agreement with the theoretical values given above but
at high fluid -.peeds the actual values are 5omewha-. greater tb~in
the theoretical, The particle size was principal"y afffctt.~d bv
three factors, The influence of film speed is well rt!prt~s~-nt~,d by
the following -xpression
xm = O~320 - 0.0028Vi mm
where x~l is the mean drop diameter; V is the spescf in m/aec,.
Agreement with theory was good, Droplet diameter was ahrays
proportional to jet diameter ard the agreement betwe(.n tbecry and
practice was again good. The angle of impact is the third wain
factor and it was found experimentally that the diameter was
greater than theory at high angles of Impact, probably because
in this case the film flows more slowly than the jet from which it
is formed. Other factors considered were of much lef:S influorct,
including the back pressure. and slight deviations from thi: (-(P~ixjal
provided that these do not greatly increase the film thlclrnc-!~s%~
The influence of the main injection parameters is much thn !~arro
when a three jet nozzle is ust-.0, In order to check the
Card 6/7

25120 S/535/60/000/119/004/009
The atcmizaci-~n of fluid E194/E435
conclusions inort~ fill-1-Y, further experimental study should be -made
of the influenczi of.' -,urface tension and other physical properties
of the liquids V.14,9!.jnrv, KzVeber and A.S.Predvoditelev are
mentioned in the paper_ There are 7 figures and 1-1. referencest
5 Soviet and 6 nin-Soviel, The four most recent references to
English language publIcation-s r-:tad as follows:
York Y,, StubbR H,, Tek M., Tranct. ASME, 1953, V~_1~75, No,7;
Fry J., Thomas P., Engineering, 1953, Vol. 179. No.7;
Hagerty W., Shea J., Journ.ApplMech., 1955, Vol~22, No.4:
Squire H., Brit, Journ, Appl, Phys,, 1953, Vol~4~ pp,_167-169~
Card'7/7

-,ACCESSION NR: AP4000401. S/0294/63/001/001/0056/0063
AUTHORS: Kull
"k, P. P.; Panevin, I. G.; nvesytik, V.~ 1.
TITLE: Theoretical calculation of the viscosity, thermal conduc-
tivity, and Prandtl number Of ionized argon
a
SOURCE: T.eplofizika vy*sokikh temperatur, v, 1, no~ 1, 1963,- 56-.63
TO~IC TAGS: argon, ionization, viscosity, thermal conductivity,
viscosity, aerodynamics, high temperature, 'gas dynamics, aigon
ionized argon
ABSTRACT: It is shown that the presence of electrically charged
particles in the ionized gas gives rise to long-range Coulomb forces.
'between the particles ,aiong with the short-range atomic forces, 'and.
this increases the effective cross sections for the elastic interac-,
tions. One of the consequences is a sharp decrease in -the viscosity
coefficient of the gas and its pressure dependence. It is also
Card 1/P
- - -- ---------

.all
ACCESSION NR: AP4000401
pointed out-=t-hat knowledge of the gas kinetic properties of gases at
temperatures much higher than experimentally feasible is of great
importance in specific problems of aerodynamics and gas dynamics.
Information is culled from a large number of Soviet and western
sources.. and the final results are presented in 4raihic'and tabular
form. Thermodiffusion effects are neglected, Origi'nal-article has
2 tables, 4 figures, and 15 formulas.
ASSOCIATION: None
SUBMITTED: 08Apr63 DATE ACQ: 13Dec63 ENCL: 03
SUB CODE: AS NO REF SOV: 010, OTHER: 026
Card 2/ft

ACESSION NR: AP4017719 S,/0294/63/001/003/0394/0398
AUTHORS., Fanevin, 1. G.; Kulik, P. P.
----------
ntal determination of the coefficient
T1TLE*. - Method for experime
of themal,conduotivity of a high-temperature gas
SOURCE: Teplofizika vy*sokikh temperatur.. v. 1. no. 3. 1963, 394-
398
TOPIC TAGS: high temperature gas, high temperature gas flow, stream-
1~ne, lunt body, critical point, molecular beat conduction, laminar
boundary layer, molecular thermal conductivity, thermal conductivity'
coefficient
ABSTRACT: An experimental method is presented which is based on the;
fact that regardless of the conditions in an incident flow aroLuid a
blunt body, the stream in a small area arouzid the critical point is
always laminar. Since beat transport transverse tvtha
Card

ACCESSION NR; AP4017719
laminar boundary layer is due only to molecular beat conduction,
measurement-of the temperature profile in the boundary layer near
the critical point and determination o
f the beat flux at this point
yields the value of the coefficients of moleculhx thermal conduc-
tivity in~i larger range of temperatures than poovaible hereto-
."'A fore. The experimental set-up has been described elsewhere (V. B.
Tikhonov, Ye. A. Yakovlev, Sb. tr. MAI, A. V. Kvasnikov, ed, Oboron-
giz 1960). The;experimental results agreed within 9% at T 12*.,OOOK:
and 5% at T = 14,000Kwith approximate *theoretical values calcuilated
by the method of W. Lochte-Holtgreven (Repts. Progr. Phys. v. 21,
!-3121 1958). It is pointed out that the method is most effective
'at high pressures.. Orig. art. has: 7 figures and 3 formulas.
~ASSOCIATIONt None
SUBMITTED a .,09.7u163 --DATE-ACQ1_. 23Mar64 ENCLs 01
;I'SUB CODEs PH, Al NO REP SOVs -002 OTHERs 004
Card

1. PANVIN" K. S.
2. USSR (600)
4. Virticulture
7. Our method for growing seedlings. Vin SSSR 13 No. 1, 1953.
9. Month List of Russian kccessions, Library of Congress, April -1953, Uncl.

. I
I 1 11 -)-%, ! II %, . __ I -
PANBVIN, V.S.- ARAKHOV, S.V.
I, :. I - ;.-j
Lvov chemapharmaceutical plant. Med.prom. 11 no.10:40-44 0 '57.
(LVOV--DRUG IOUSTRY) (MIRA 11:1)

I PAVLTIN, I,hf 1~ , -
Young specialists In charge of important sections. Obahchastv.
Pit. n0-9:12-13 6 '59. (MIRA 12:12)
1. Direktor Belgorodskogo tresta atolovykb, kafe I restoranov.
(Belgorod--Restaurants, lunchroom, etc.)

PANEVIN. V.S
Compressing the taboret seats made of wood waste. Bum. i der. prom.
no.1:38-39 Ja-Mr 164. (MIRA 17:6)
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. ;oil. "tablislwd tKtvmeu colli%hens of tht. ft"I
let tel"Is of "
andwevondkind. The drop of rimit-srek truip. with cut.
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FANEVNI14, K.
L
-Excitation 0l -atoms In
and experimental (lata on the Influence of current on concu.
Of OxtlkCJ BtOMS in rare-gas discharges (He Ne, and A) sto
critically discussed. Existing datik and pro(~ measutements 7
Indicate that the dep9ndence of concn, of excited ritoms on
current Is determined by varladon In the electron iemp,
with current. With Increase of current the electron ternp.
falls but the electron concn. tncrcatc5. The superpoRition of
these two factims gives a rnax. for the no. of exclUng collisions
with a certain ma ultmde of current at- which satumtion
ccacn. of the . excited atoms occurs. Previous theories
Assurne shortening of the life of excited atoms by collisiong'
of a de-activating type whilst from the viewpoint presented.
-A~o life Is Consi( W_ R. A.
--- --------
;4a,

Plil'T."waill, Y. 1. - -
"The -T,'xitation of Atoms During a Discharge in Inert Gases,"
Iz. Ak. llaulc SSSR, Ser. Fiz., 4, iio. 1, 194~0.
Dept. of PlWs-Acs, V. '11. 11-11olotav Inst. of Power Engineering, 11-loscowT

PIOEIVIN, l,'Iadimir Semenovich; FCI'UL'IiITSI',IY, Ilikolay Mikhaylovich
M.M.); DOROSIMIKO, M., rGd.; Y.EDOVIZ, S.,
tekhn. red.
[Standard-bearers of comimist laborlPraporonostsi komuni-
stychnoi pratsi. Llviv, Llvivslke knyzWovo-zhurnallne -,'Yd-
vo, 19161. 53 P. (Lvov--Drug industry) MULk 15: 11)

-~M - -
PANEMbl) K. I. ., Enrtr. Cand. Tech. Sci.
Dissertation: "'Excited Atoms in the PoE:itive Discharge Colurm of a, Fluorescent Lamp."
I'loscow Order of Lenin Power Engineering Irst irieni V. M. Molotov, 20 Jun 47.
SO: Vechernyava Moskya, Jun, 1947 (Project #17836)

Metastable stem In the finoreseAst lamp: 9.11auevk1o
(mohmw Inst- and Alfun;ons Blectroiech. bmin-Irme,-,
Moscow). PAIddy Akek Yeah S.S.S.R.- 59, WA
(INS): Oita. ZmIr. (Rualan 7one Ed.) 190. U. 1262,
The life perW of ezdtod Hg atom& in the poa. column of tbe
diwhaW of a dunerwat larnp was deW. under normal
operating coaWtions (SW ma.. vapor preesure of US 0.01
mm.. diam. of tube 30 inm.. A pcessure 4 mm, Hg), 'the
foHowins values an nvwted for the "crest states: #31P.
4 X 10-11. 61P. I X 10-1% 6*P# 6 X 10-0 me. Theve vahs"
coffeWood to thoet c". for colikions of the 2nd type with
eketrous. 7UInte"tyoltheUne2&77A..washO.S%of
the clec. out Imt of the lamp: of the fine 1850 A., only 25%.
In the Abseocr of A the intensity of the line 2337 A. waA
about 76% 1cm; the line WO A. was unaffected.
M. G, Moore

ACCESSION: NR: AT4017003 S/3057/63/000/000/0144/0147
AUTHOR: Tikhomirov, V. a.; PanevkIna. Ye. A.
TITLE: The use of epoxy shieldings for protecting metal and concrete surfaces
SOURCE: ZashchitnyVtye pokryftlya v atomnoy takhhIke (Shielding In nuclear engineer-
ing); sbornik statey. Moscow, Gosatomizdat, 1963, 144-147
shielding, atomic reactor
TOPIC TAGS: epoxy resin, corrosion, nurplear shieliiing
epoxy shielding, radiation protection
1 ABSTRACT: Shieldings made of epoxy resins are the most widely used protection
against corrosion for buildings, communications, and equipment, Including nuclear
devices. In the U.S.A epoxy Ihieldings areused to protect steel and concrete
I surfaces from a radiation of 105 red and the simultaneous action of boiling watero,
I of the resins being manufactured In the Soviet Union, the high-molecular epoxy
resins can be used for nuclear shielding. This type of epoxy resin has the best
physical and mechanical properties. Different compositions oi epoxy resins and
solvents are listed in the article. Both air and heat drying can be used for them.
An addition of 1% of melamino-formaidehyde resin is used to lower the surface
i tensicin of the epoxy compound, thus imprcving the coating. The viscosity of the
resin ii also important for the coating method. Coffwwn spray guns can be used
Card

ACCESSXON KR: AT4017005 8/1-057/63/0001000/0154/0157
AUTHOR: Panovkina, '~o. A.j Tikhomirov, V. D.
TITLE; Investigation of the vortex method for applying polyethylene shit'ldin,';
to.metallic objects
SOURqE: Zashchitny*ye pokry*tiya v atomnoy tekhnike (Shielding in nuclear on-
,gLneering); sborrkik,statey. Moscow, Gosatomizdat, 1963, 154-157
TOPIC TAGS: polyethylene, polyethylene shielding, vortex coating method,
nuclear ahielding
ABSTRACT: Folymersand low-molecular resins are widely used for shieldings,
'obtained by the vortex coating method. V. S,. Shifrin and N. N. Samosatskiy
published an article about this method (Polietilen, pererabotka i primeneniye.
L., Goskhimizdat, 1961). However, the laws of vortex atomization were not clearly
specified in the article. The present investigation sbowed that the hydrodynamic
laws for common su?pensioa layers are applicable. Low-pressure grade T-085
polyechylene was used with particles of 200-300 'mm and a moisture content of not
Over 37.. The surfaces were first cleaned of rust, scale and dirt. The parts 6
were heated in an.6lectric oven to.350-400C 0 malt the polyethylene. (See
Card 113

.ACCESSION NR; AT4017005
0
Fig. I of the Enclosure.) Stialle,r articles werg,heated to higher teipperatures,
due to the higher 66~ling rate. .,For,,a 200-250/4,.co~ting the article.was lowered
into the bath for 740 seconds. The;,polyethyleqp coating resisted tMperaLuree
as low as-50C. es well as ^407. nitric,,acid, 307. hydroobloric acid, 36% sulfuric
aced, 35% hydrof lu?,ric acid, 907.. formic acid, at 20-6-OC, and alkalis of various
concentrations. T~q tests were performed for 2 to 12 months. The authurs
conclude that the yQrtex method will.be widely used for coating polyethylene -1
ch6ical equipment,.,tools, instruments, and materials used for constructic~n.
The apparatus requir .ed for coating suspensions' can be made at any factory having
a machine shop. Orig..art. has: 3 figures'and 2 equations.
ASSOCIATION: None
SUBMITTED: 00 DATE ACQ: 2OFeb64 ENCT-.: 01
SUA CODE., OCLN NO RZF SOV: 000 OTHER: 000
Card 2/3

'A'CYSSION NR.- AT4017005
ENCLOSURE: 01
to
too
Zoo
N
40 So 00 ILV
'Duration of otupension, see.
Fig. 1. Relationship between T-085 Polye~thylene coating surface,
the duration of auspenaion and heating temperature.
Card-3/3

Distrz.
x4r,

VASILOYOV., Va--iliy Vassillyevich; KARMAI , Mhail Mirovichl-TAIMMM,-
Pikolay Petrovich; ZHIINAKOVA, 0., red.; ISUPOVA, It'.. tekIL-.
,__ ~r. ~~
[Collective fnrm on the upsurge]Kolkhoz na podnems. Simfe-
ropol', Kr~mizdat., 1962. 30 p. (KRA 15:11)
(Col.lective farms-Management)

PAIIEYAKH , B .. P.
Bxtensicwis of some differential operators. Sib. mat. zhL,--,
2 no.4:574,-581 JIAg t6l. (MIRA 14:9)
(Operators (Mathematics))

MEYM
Some problems in harmonic analysis. DAL AN SSSR 21+2 no,5alO26-
1029 F r62. (MM i5s2)
1, Mokovskiy rqudarstvennyy universitet im. M.Volomonosovao
Predstavleno, akademikom P,S.Aleksandrovym.
(Harmonic analysis)

PANEYAKH, B.F.
General systems of differential equations withbonstant, coefficientAi.
DOkloAN 86SR 138 no.2t~97-300 W 161. (MIRA 14:5)
1. M.,oskovskiy, gosudarstvennyy univeristet im. N.V.Lomonosova.
Predstavleno akademikom A,N.Kolmogorovyme
(Differential equations)

GORDINGP Lare [Gardin6L3;jWEYAMj B.P. Itranslator); DBZ-IN9 A.A., red.j
SHIROKOV9 V.F.p redo; KHARIMUMA9 L.v tekbn. red.
(Caucb;rlo problem for Wperbolic equations] Zadacha Koshi. dlia
giperbolicbeskikb uravnenii.'Pod red. A.A.Dezina. Moskva, Izd-
vo inostr. lit-ry, 1961. 120 p. Translated fr4m the English.
WRA 34:8).
(Differential equations)

PAUYAKH, B.P.
Axistenee and uniqueness of a solution for the n-metaharmonic
equation in unbounded space. Vest.Moak.un.Ser.mat., makh.,
as".-ron.gfiz., khim. 14 no.5:123-135 '59. (MIRA 13:8)
(Harmonic functions)

6909
S/055/59/000/05/01-e-.,,'020
AUTHOR: Paneyakh, B. P.
TITLE: On the Existence and Uniqueness of the Solution of the
n-Metaharmonic Equation n e Unbounded Space
PERIODICAL: Vestnik Moskovskogo niversiteta. Seriya matematiki,
mekhaniki, astronomii, fiziki, khimii, No. 5,
pp. 123-136
TEXT: Let the n-metaharmonic equation
(M) P ( & ) u = i~~ u + a, - L~- 1 u + . - . + a u ~ f
be given, wher-i a4, . . ., a.-are complex numbers, a, + 0,x
point ol the space R. and f(-X") a finite function. Let (M) be
written in the form
IV V S
(2.20) JT u = f
The main,result of the paper consists in the statement that there is
a unique solution of (2.20) which is a-linear combination with
constant coefficients of the solutions of the equations
Card 1/2

6909
S/055/59/000/05/012/020
On the Existence and Uniqueness of the Solution of the n-Metaharmonic
Equation in the Unbounded Space
(2.21) + 00 = f (k = 1. . kc)
U~t
and
(2.22) t u L+0 = f (t = 1, .
The solutions in question of (2.21) and (2.22) are determined by cer-
tain conditions (order of growth). There are 10 theorems and 4
lemmata altogether.
The author mentions J. N. Vekua; he thanks G. Ye. Shilov for the
subJect and advices.
There are 4 Soviet references.
SUBMITTED: July 3, 1956
Card 2/2

34820
q;2 0 0
AUTHOR:
TITLE:
PERIODICAL:
Faneyakh,__]3_.
Some problems of harmonic analysis
S/020/62/142/005/009/,122
B112/B102
kkademiya nauk SSSR. Doklady, v. 142, no. 5, 1962, 1026-1029
TEXT: The author describes sets VwhioA fulfill the condition
up (fj,(~)12 )1/2