SCIENTIFIC ABSTRACT SIDOROV, B.N. - SIDOROV, F.F.

• Document Type: CREST
• Collection: Scientific Abstracts
• Document Number (FOIA) /ESDN (CREST): CIA-RDP86-00513R001550510007-7
• Release Decision: RIF
• Original Classification: S
• Document Page Count: 100
• Document Creation Date: November 2, 2016
• Document Release Date: August 23, 2000
• Sequence Number: 7
• Publication Date: December 31, 1967
• Content Type: SCIENTIFIC ABSTRACT

N KOV , ii. V . ; ~; Ilikk(N p B. 14.
Aut-,rnatir single-chain OAFF elevat,~,r for bottle corive./ing
beLween floors. Trudy Ukr!I[ISII no.9:145-150 '64.
(IMIRA -17: 10)

USTIKENKO, V.F.,, starshiy dorozhnn mig ter; ZIKOV) F.M., starshiy doroxh-
nyy znp ter; KIREY, P.I.; ITANITSKIY, M.V.; IDUMV, Te.I., doroub-
nyy master; GAYDAR, P.R.;-5ID=T,-B.Ns-,- SAVKOVp Maj.; SAFOIKU,
A. W. ; PETWV,, A. S, ; BURLAK, F. V.,, insh.
letters to the editors Put' i putkhoz. 5 no-5,42-44 MY 1610
(MIU 14:6)
1. Stantsiya Kupino.Onskov. dor i (for Ustimenko). 2. StsaUiya
Koteltnich, GorIkovskoy dorogilfor Zykov). 3. Stantaiya Fetro--
pavlovok., (bakoy dorogi (for Kireyp Ivnitskiy). 4. Stantelys
Stupino., Moskovskoy dorog:~ (for liobanov)s 5. Zuwstitall n4ichall-
Afta distanstBii puti, at., Izyum, DDnetskoy dorogi (for, Gaydar)e
6* Machaltnik distantaii Imti, at. Berlik, Kazakhskoy doroci
Oor ftdorov)e 79 Naohallnik PMS-629 ate Nikitovkaj, DDnetokoy
dorogi (for Saykaw). 8. 4isbW master shchebenochnogo kar'7w&
at. Chokpar, Kazakhokoy darogi (for Safonkin). 9. Nachallnik
tekhnicheakago otdela alushby puti,, g. Yaroslavl' (for Petrov).
10. Distant5iya zaahchitnvkh lesonaaaxhdeniy, at. Artemovskv Do-
netakoy dorogi (for BurlAd.).
(FAilroadw)

SIDOROV$ B.N. (Alma-Ata)
Improving the organizatior-cf work* Put' I put.khoz. 8 no.4:12-
14 164. (MIRA 17:4)

SRLPOSHNIKOV. V.N., akadamik. radalctor; IrONDRATITEVA, 1.11. [translator];
HEIMIYEVA, V.L. Etranslato:.-I; SIDOROV, B.N., redaktor; INIW, H.G,#
radaktor,- SHAPOTALOV. V.I., takAlf-MMt-foidaktor
[Bacterial physiology. Tranulated from the Inglishl Fisiologita
baktarii. Perevod a angliisl:ogo I.N.Irondratlevoi i VA.Mekhtievoi.
Pod red. i a predial. V.N.Slispoohnikova. Moskva. Izd-vo Inostrannol
lit-xy, 1954. 547 P. (KU 7:11)
(BACTIRIA)

~ KHVOSTOVAq V.V.
Factore influencing the genetic offect of ionizing rodiatiow.
Itogi nsuki% Biol. nauki no. 3-.]!,16-227 160. (KIRA 13%10)
(RADIATION-PHYSIOLOGICAL EFFECT) (VARIATION (BIOLOGY))

I)LJBININ, N.P.; SIDOROV, B.I.; SOKO'.WV, R.N.
Experimental analyi3is of the primar7 mechanism of the effect
of radiatioh on cell nuclei. Dok*-'.Al SSSR 133 no.1:221-224
Jl 160. (MIRA 13:7)
1. Institut biofisiki Akadenii nauir SSSR. 2. Chlen-korrespondent
AN SSSH (for Dabinin).
(RADIATION-PUSIOWGIUL JFFBCT)
(CEWMDSOMES)

',SIDOROV, B.N.; DUBININ, N.P.; SOK01OV, N.N.
Exp,~rimcntal study of the ;.-ole of free radicals and the direct effect
in the primary mechanism of the radiation effect. Radiobiologiia I
no.2:161-171 161. (MIRA 14-7)
1. Institut biologicheskoy fiziki AN SSSR Moskva.
(RADIG= (GHEM11STRY) I
(RADIATION-PHM;IOLOGICAL EFFECT)

3331!',
S/560/61/000/010/013/016
27, 12-"0 D299/D302
AUTHORS- Sidorov, B. N,, and Sokolov, N. N.,
TITLE: Effect of space-flight conditions on the seeds
of Allium Fistu.losum (winter onion) and Nigella
Damascena (ranunculus)
SOURCE-~ Akademiya nauk SSSR. Iskusstvennyye sputniki
Zemli. no. 10. Moscow, 1961, 93-95
TEXT- Dry seeds of the radicsensitive A. fistulosum and of
the radiostable N. damascena were investigated, From a table,
it is evident that the A. fistulosum is 9 tin-es more sensitive
to X-rays than the N. damascena. A comparison of the number of
aberrations in the seeds which took part in the flight with con-
trol seeds showed no difference whatsoever in the frequency of
chromosome rearrangements in the seeds under investigation,
This negative result, obtained %ith dry seeds, made it necessary
to conduct tests with growing seeds, These tests showed that
Card 1/3

33315
S/560/6-/000/010/013/016
Effect of space-flight... D299/D302
space-flight conditions have a Stimulating effect on the growth
of both species; this stimulating effect is mcre noticeable in
the radiostable species N. damal3cena. In general, dry seeds are
fairly stable to ionizing radiation; thus, the seeds of A. fiatu-
losum have to be irradiated by a dose of 250 - 500 r, and those
of N. damascena by several thoutiands of r6ntgen in order to
observe an actual increase in chromosome rearrangements. The
authors arrive at the conclusion that the increase in the growth
of the seeds cannot be related -;o stimulating radiation doses,
as the stimulating effect is stronger in the radiostable species
N. damascena and weaker in the radiosensitive species A. fistu-
losum, If the observed effect on the N. damaecena would have
been due to radiation, the indicated dose would have caused
chromosome aberrations in the A. fistulosum to3. This was, how-
ever, not observed. It is evident that the reason for the ob-
served effect should be sought :.n other factors which are active
in apace.-flight.--factore which are thoroughly unlike those
Card 2/3

COtt I I 011M I tr I "cc" I be F H- POte" I I., I of I IM I I M I, It of( ricket I I )rrh'K If r .4 W On -I I. it
V.
A --chod h3% e~crs &~tknvd to dverotine the redo% j%nenlial of the h&emv'y,rh of Ow~ In i,o. The
Ir!" t of -r,oui rletec to v fit I - -m (h YTv - -j. It, t,!cc I n r suSi arcr% V t v
h., tven lr.~C'og-frd.
I~ncvrtrhord sf,'r-mes in the vtil~ or 4e reo., r~ot-1.1 hatc, been ohsc~v' tor or
tut.1.1's- -4 for IMocl into which rr-sim ive substoocts had been immiltited On the other hand. when
rrolevike , ot,,13"c" are introduced into the iijainitin during hypow. the Values v~ the rc4ot rotential exactly
correlate itith the nuitnitudc efthe protective tffcct and ridioscrivitylty, The dAia Mvned in the literature which
failed to %how tuch correl3tton wIrre obtained then the pnential was m2sorcd in vi - am did reit allow For the
I'ttiq'fNglon o(the 'St" reaviont in Ini"Ittyltemn, Offered '?I the rrote-fitc cfrcc(4.
%1.1. At-., VIVO V
(411
Direct mod lodirer Bottler" D.-Its, to the C.11 .14-1-o
N. P. Dabl"K IL N. Swett" anill M K. ~.Ioslov
It is known that molecules in squinous solution can undergo radiochcrivicst rc*ai3m due to fier radicals from
the radinlyin of water. (v by -litect energy abtorption.
The trenetv of free radicals froduccd chemically within the cell IFeroon reaction. reavion of
i
Sworbic acid with hyd'_'t" allow- u% to assets the importance of the direct end indimt rvidiatiors
'frrrtI- h ....... -, It -I shown in pf.,t "III trootlcts 44 Alliansfivolmobt) :hat substarcm which rrotect
Ibechromos,"es front the effect ofthe free rAlicalAoll and 110. obtained themicat'llriK, Kill. hy"uIrItlic.etc.)
or not protecloc when the chromosormi sit itradialcil with X-ray*. We cosclole that the Irricitc effect of
"eWw" It 4,,c ro-A"Ir In Itte direct effect Joe not to the 9troducts of *$fee recriolrit.
I"Arvilcl t.periments with DNA solutions M. 1. %teltiherikov) showed that the crccti%cncs% of the dirftt aclic-is
on D14A is much greater Ilion that or the indi vct effect.
ThewnsidvabIc rrotmttwobility of iubilmrc" which protectchn~osomicsfrom !irtnidivols was dc~rovrsttd
in solution% of DNA o,nly at low, DNA In solutions with high DNA corscwtstiovt the girviccit"
effect is i,tnally xbt-C which ipomti to the Ctedorninant r6k of the direct erect.
A~_ W T'~. W'U VSS'#. At-
report presented at the 2VA Intl. Cmgmwe of RadJAIL141111 I"Owliv
Harro, - 5-1.1 AU8 1962
_~ntat/rorkvklre, Gt. PrIt.

SIDOROV, B.N.; SOKOLOV, N.M.
Effect of tho'conditions of space flight on the needs of Allium
fintulosum and Migella damincem. Probl.kona.biol. ls248-251
162. (WRA 15 s 3-2)
(SPACE FLIGHT.PHYSIOU)GICAL EFFECT) (SEEDS)

KHVOSTOVAP V.V.; PROKOFIYEVA-BELIGOISKAYA, A.A.; SIDOROV, B.N.;
SOIKOLOV.9 N.N. C-- ~
Effect of the conditions of apace flight on the seeds of higher
planti and on actinomyces. Probl.koem.biol. 2:153-163 162.
(MIRA 16.-4)
(SPACE FLIGH11-PHYSIOLDGICAL EFFECT)
(FLATS) EFFECT OF SPACE FLIGHT ON)
(ACTINOMYCES)

SIDOROV, B.N.; SOKOLOV, N.N.
Radiation analysis of chromosome discreteness during the
process of autoreproduction. Radiobiolog:Ua 3 no-3:415-419
163. (MIRA 17:2)
1. Institut biologicheskoy fiziki AN SSSR, Moskva.

ADOROV, B.N.; SOKOWV, N.N.
Lysis of chromosomes and the blockade of The spindle. Biul.
MIP. Otd. biol. 68 no.5:78-91 s-o 163. (KrRA 16:10)

SIDOROV, B.N.; SOKOLOV, N.N.
Lysis of the ebromosomes accompanying spindle blockade. Dokl.
AN SSSR 150 n0-3:653-656 My 163. (MIRA 16:6)
1. Institut biologicheakoy fiziki AN SSSR. Predstavleno
akademikom V.N. Sukachevym.
(Chromosomes) (Karyokine;919)

Sjf',C)POU, .,:; *, ; ~ '"'i ", ~,,,L.. ..
1. 1 - D. N. ; SOKOLO"i. !!. ~: . -, I .- - I . ..-' 0
~ I - I -- "
I
Mutagenic effoct. cf :-, a :, e,~nerationn.
GerietJka no.1:112-122 18;10)
1. Tn,;tltut biclcrJ-".,-,-,-., P!Z~ I
u - , - - ?l. - " - ~, ~ 1, i. A N, S, S -~~ 1~ , --'; ."Va a

Radlatlon arilysis of the ntructure
Radloblolog-a 4 no.6i828-835 164.

SIDDROV, B.N.; SOKOLOV, N.N.
Spindle blocking as a cause of the formation of polymorph:ous
nuclei in polyploid cells. ISitologiia 7 no.5,645-650 ,
S-0 165, -Cj#Ws12)
1, laboratoriya radiatsionnay genetiki Instituta biofiziki
AN SSSR, Moskva. Subuittod August 10# 1964.

'1WROV, B.S..inzb.
Draft of now norms for determining costs of nachinery spare parts.
Stroi. truboprov. 5 no.10:29 0160. (14IRA 13:10)
(Building machinery-Equipment and supplies)

SIDOROVE-PA... inzh,
Amortization allowances for machines. Stroi. truboprov. 6 no. 2:25
F-161, (MIRA 14:5)
(Pipe~lines-Accounting)

SIDGROV, B.S., inzh.
Econcmic basis for choosing pipe-carrying machinery. Stroi.
truboprov. 7 no.7:28-29 Jl 162. (MIRA 15:7)
(Pipe-Transportation)

SEMENOV, B.N., kand.takhn.nauk; SIDORIN, .. B.S., inzh.
Study of the efficiency of usting transportation facilities for
moving pipes. ?rudy MIST no.14M4-1233 162. (KRA l6sl2)

SIDOROV, B.S., inzb.
New stagdards for amortizatior. deductions for machinery in pipaUnp
constructioA. Trudy VNIIST n(,.11+sl05-113 162. - .. -~-
Technical and economic analysis of the efficiencv of machines for
cleaning pipes with a diampter of 72Q and 820 m. lbid.aI64,168
(~ff RA 16 -.12)

SIDGROV,D.
Ut' build out of brick. Sell.stroi. 10 no.7:16 T1,55. (NLRA 8:10)
1. Nachallnik otdola po stroitelletva v kolkhozakh Nikhaylovmkogo
rayon&, Novosibirskoy oblamtI
(Nikhailovka District--Building ia&stry)

SIDOROV, D.A.
Repairing metal bridge spans. Pul' i put. khoz. no.9:18 S '58-
(14IRk 11:9)
1. Nachallnik otdoln tub"nernifth sooruzhenty, Leningrad.
(Railroad bridg"s-Main"anance and repair)

SIDOROV, D.A., inzh.
flew method for repairing abutments. Put' i put. khoz. no.5:19-20
K7 '59. (MIRA 12-M
(Railroads-J(aintenance and repair)

VOLKOV, P.F.; SIDOROV, D.A.
Ramedial treatment of embankmento. P'it' i put.khoz, 4 noo6:19
Je 160. (MM 13:7)
1. Starshiy inzhener distantaii puti, stantsi7a Chudovo, OictyabrlskG7
dorogi (for Volkov). 2. Nazhallnik otdela inzhenernykh sooruzheniy
sluzhby puti, stantsiya Chudovo, OktYabrlskoy dorogi (for
Sidorov).
(Embankments--Haiatenance and repair)
(Railroads--T~rack)

SIDOROV, D.A.,.-inzh. (Leningrad); POMOGATIV. P.ye., in2h. (Leningrad)
Kaintemance and repair of mansive brbIP anbetructures. MI
i put. khoz. 4 no. 12:28-29 1) 16o. (=A 13t12)
(Railroad bridges-Maintgnance and repair)

AID P - 1943
Subject USSR/131ectricity
Card 1/1 Pub. 29 - 23/31
Authors Yecheistov, N. K., and Sidorov, D. F., Engs.
*WAIM'" -.A-,
Title Complete apartment panelboard
Periodical Energetik, 3, 28-29, Mr 1955
Abstract The authors describe the panelboard designed by the
design division of the city's Metro Transportation
System. They give all data concerning dimensions,
equipment, and performance. One detailed drawing with
connections diagrati.
Institution: None
Submitted : No date

SIDOROV.D.7.,
, apartment electric control box having three circuits,
and safety fuses. Gor. khoz. Mosk. 29 no.5:38 My 155.
(Wattmeter) (Blentric fuses) (MLRA 8:6)

SIDDROV, D.P., litzhoner.
Hook for uprooting tree stumps. Torf.prom.3~ no.505-36 056.
I.Shaturskeye terfoprodprlyatiya. (KM 9:9)
(Hooks) (clearing of lands)

SIDOROV, D.P.; SLASTENOV, Yu.L.
Stratigraphy of Mesozoic coal-bearing sediments in the Ust'-
Vilyuy gas-bearing region. Trudy VNIGRI no.186:32-43 161.
(MIRA 15:3)
(Verkhoyar.sk Range-Coal geology)

SIDOROTO B.A., lash.
Applicability of the laws of Newton and PirrIer to the calculation
of frictloa resistance and bea,% ezeh&mSe taking place on the surface
of a body washed by a streamiflim. Thpleenergetika 4 se.12:73 D 857.
(Fluid trawdes) (NLU 10ill)

AUTHOR: J91DOR OV-,-Fr-s-A - i - PA - 2128
TITLEt On the C-o-n-sIderation of the Influence exercised by the Non-Iso-
thermal Flux in a Laminar Current of Liquids which are Capable of
Dripping in Tubes.
PERIODICALs Zhurnal Tekhn. Fiz., 1957, Vol 27, Nr 2, pp 327 - 330
Receivedt 3 / 1957 Revieweds 4 / 1957
ABSTRACTs The object of the present work is to find an approximative
equation for the field of velocity and the temperatures in the
case of a laminar current in tubes with liquids which are capable
of dripping in consideration of the changing of the viscosity of
the liquid with respect to temperature. This investigation was under-
taken for the purpose of showing that the modification of the
physical characteristics of liquids with temperature is one of the
most important causes of the divergence between theoretical solu-
tions and experimental results. At first the equations for the
motion and heat transfer in the boundary layer of cylindrically
shaped tubes are written down. The existing solutions of this
system of equations apply only to the case ofp& - const, which
leads to more or less grave errors. Therefore, the attempt was
made to find an approximated solution for this system of equations
for the case that the change of the viscosityttin connection with
temperature is taken into account. The method of successive ap-
Card 1/2 proximaticn by SHVETS-TARGA was selected for this purpose. At

PA - 2128
On the Consideration of the Influence exercised by the Non-lao-
thermal Flux in a Laminar Current of Liquids which are Capable of
Dripping in Tubes.
first, temperature distribution in first approximation for the
radial cross section of the boundary layer of the tube was found.
Next, the temperature dependence of the viscosity coefficient of the
liquid capable of dripping is showr- with the required accuracy in
form of a series. In practice the jolynomial of the third, or
even only of the second degree will suffice. After transformation
and integration the equation for the velocity of the flux in the
case of a nonisothermal motion in the tube is obtained. Next# the
formula for the average velocity of' the cross section is given,
after which only the domain adjoining the wall is investigated
and the equation is found in which one of the multiplicands taken
the influence exercised by the non-isothermal course of the
current into account. In the case of the second initial equation
the case of an infinite distance from the wall As dealt with and
an ordinary differential equation is obtained. The average value
Card 2/2 of the heat current passing through the unit of the surface of the
tube is written down in form of a formula.
ASSOCIATION: Not given
PRESENTED BYs
SUBMITTED:
AVAILABLE: Library of Congress.

AUTHOR SIDOROV A~ PA - 2547
o
VC
TITLE o~relation between Surface Friction and Heat Exchange.
a th
e
(0 svyazi poverkhnOBtnogo treniya a teploobmenom.- Russian)
PERIODICAL Zhurnal Tekhn. Piz. 1957, Vol 279 Nr 3, pp 560
566 (U.S.S.R.)
;w
Received: 4/1957 revi ed: 5/1957
ABSTRACT Though the theory an the analogvs phenomena on the oocasion of
the transmission of momenta and 4nergy in relation to the
quantitative partf which was for the first time mentioned by
Reynoldsq was named the hydrodynamic theory of heat exchange,
the author believes that it ought to be called the theory of
thermofriotion analogy. The reason given for this is that the
main task of this theory in the discovery out of a direct
relation between the hydrodynamic and the heat exchange
characteristics. Existing methods are not complete and re-
sults differ up to 100 % and more. A much more simple and
safe way is shown here. At first the universal relation bet-
ween Nu and Re is deduced:
Nu I c Re 9-1 ..... dimension/less
2 f 0 t0 temperature
u
- ....dimension/less
U velocities
CARD 1/2

PA - 2547
On the Correlation between Surface Friction and Heat Exchange.
of .... coefficient of surface friction, dimensionless.
The value here acts as second parameter. The determina-
tion of this V%-Ivcj-ives the solution. Since a laminary sub
layer exists in the turbulent boundary layer the value of this
parameter can be assumed to differ only little from that of the
laminary boundary layer. This value can be found analytically
fan,,the laminary boundary layer. It is derived here and the
basic equation reads as follows:
NU cfRe Pr 1/3-
Now this formula for the different cases of a turbulent flow
is applied and it is shown that the results obtained agree
with those of the experiments. The same is shown to be the
case with motions of liquids in tubes as well as with the
motions of a compressed gas. The last mentioned formula
remains the same for gases. (With 2 tables)
ASSOCIATION: not given.
PRESENTSD BY: -
SUBMITTED: June 30th, 1956.
AVAILABLE: Library of Congress.

I;IIYT-(.)V, E.A., G;Ind Fecti 'jci -- (dis5) "Certain problems
--r(t
of' I.ne L:ieory of convective and radA hPit excnang-e.,,
on, ril-lb itoiise of Acad .,ci (JS).,;L(7, 9 p!)
M
I
(A(-,,,jri Jci US R. Power Engineering In3t im G.V.
Krzhiziianovskiy) 185 copies. List of authnrls works
DI) 8-9 (1]. titles)

SIDOIK)V. R.A,_ .
Contemporary mnthods in ennyaction heat transfer thoory and their
application, Inzh.-fiz.zhur. nn-5:62-70 MY 158. (MIRL 12t1)
1. Finargaticheakiv institut A3 SSSR, g. Moskva.
(Heat--Transmission) .

SIDOROV, B.A., insh.
A valuable book on the theory of convective heat exchange
(07oundations of the theory of h9st exchangeQ by S.S. lutateladse.
Reviewed by B.A. Sidorov). Enerlomashinostroonie 4 no.11:43
N 058. (KIRA 11:11)
(Heat exchangers)
(Kutateladso. S.S.)

AUTHOR: Sidorov, E.A. (Moscow) SOV/24-58-9--18/31
TITLE: -Convective Heat Transfer UndEr Non-stationary Conditions
(Konvektivn,yy teplccbmen pri nestatsionarnom rezhime)
PERIODICAL: Izvestiya Akademii Nauk SSSR, Otdeleniye Tekhnicheskikh
Nauk, 1958, Nr 9, pp 116 - 11? (USSR)
ABSTRACT: Non-stationary convective heat transfer is met with in
many branches of teohnology. The non-stationarity may be
associated with the process i-~self or with a transition
state from one stationary process to another. In spite
of the major practical importance of non-stationary thermal
convection, there are no theoretical or experimental data
on the subject at the present time. The absence of such
data is due to the great mathematical difficulties involved
in an accurate solution of the preDlem. This is thq reason
why in calculations of heat-transfer processes in which
speeds and temperatures are functions of time, one has
been forced to use forn-uiae which describe stationary
convection assuming that these formulae will also apply
when the speeds and temperatures which enter into them
vary with time. However, there are no data in the literature
which would indicate the range of applicability of these
Cardl/5 formulae. The present paper is an attempt to obtain an

SOV/24-58-9-18/31
Convective Heat Transfer Under Nc,n-stat,'r,,nar,7 Conditions
apprcximate solutien of the
convection,, In calculation
a medium in which ccnveo~tion
the basics energy equanion. in
be written in the farm:
prrblem of non-stationary
of head transfer between
ta.~:es place and a surface,
a I Ver nea-r the surfaae may
t ?)
+ U - 4- 7
ax
0 .1
Card2/5
Here u z;~-_d -.r are tile of the velocity vec~tor
along the x and Y ~~es whi~,~i with the direction
of flow and the normal to the 7j:-.-facG respectively,
i .. - difference between a point in
t = T-T Ls the temperat-ir-= -_
the layer and the surface, -t is the time and a is the
coeffir,ient of "temperature c;ondL.CtiVity". In the zero-.
order approximation on-'.y the conductive term is retained.
On solving the equation-.
2.,
I " () (2)
ay

SOV/24-58-9-18/31
Convective Heat Transfer Under Jon-stationary Conditions
in which convection is taken indirectly into account via
the boundary conditions:
t = 0 for y = 0, t = t . for y (3)
we find:
t = toy/15 (4)
where 6 is the thicsness of the layer, t = T-T and
0 0
T0 is the temperdure of the main current. Substituting
this expression into 3q (1), in which only convective
terms are now neglected, we find the equation which takes
into account the non-stationary nature of the phenomenon
in the first-order ap-?ro imation:
a (5).
y 0)
On solving this equation, one finds that:
Card3/5

SOV24-58-9-18/31
Convective Heat Transfer Under licn-stationary Conditions
q ec-ht02 ( to, U)
- = 1 - --= + (8)
qo E)q0 to
where q is the thermal flux through the surface in the
non-stationary case und q. is the flux under stationary
conditions. It follows that the formulae describing the
stationary process wi--,.l hold approximately provided:
eck t' U1 (<
i_;7
C (700
(10)
where and c are the density and specific heat,
respectively and u is the velocity of the main current
beyond the layer near the surface. For laminar flow
Card 4/5

SOV/24-58-9-18/31
Convective Heat Transfer Under Non-stationary Conditions
m = 1/2 and for turbulent flow M = 115 . The
prime indicates diffeientiation with respect to time
and m0 = q 0/t0 .
SUBMITTED: February 27, 1957
Card 5/5

24(8)
.%UTHOR: Sidorov; E. A. SOV/57-58-12-10/15
TITLE: On the Influence of Non-Inothermicity on the Hydraulic Drag
in Laminar Motion of Drop Liquids in Pipes (0 vliyanii
neizotermichnosti na gidravlicheskoye soprotivleniye pri
laminarnom dvizhenii kapeltnykh ~hidkostey v trubakh)
PERIODICAL: Zhurnal tekhnicheskdy fiziki, 19R8, Nr 12, pp 2711-2712 (USSR)
ABSTRACT: The results obtained previously in the paper cited in
reference 1 are :ftfther developed, made more
precise and compareC with experimental aata. In order to
check furmula (4) specifying the heat flow between the liquid
and the wall of the tube the protlem of the influence of the
direction of a heat flow-is inveetigated. The influence of the
non-isothermic courset on the-hydraulic resistance is then
examined. It is shown that formula (a)-is a generalization of
formula (9) establisl~ed by Poiserille (Puazeyl~)-for the case
of a non-isothermal motion. The relative of I coefficient of
hydraulic drag) in tEe case of a ehange in direction of the
heat flow was calcultted. Water was used as fluid medium and
for the calculation of the coeff!.cient of the non-isothermicity
Card 1/2 formula (5) was employed. It is shown that for the hydraulic

On the Influence of Non-Isothe,rmicity on the SOV/57-58-12-10/15
Hydraulic Drag in Laminar Motion ct Drop Liquids in Pipes
drag the difference between the theoretical and experimental
values does not exceed 1 %. There are 3 references 2 of which
are Soviet.
SUBMITTED: December 20, 1957
Card 2/2

AUTHOR: Sidorov, E. A. Engineer. 96-4-15/24
A method of --,lloviin-- for unstable conditions durin~E
convectiva heat excaan(Se. (Uchet vliyaniya
.1
nestatsionarnooti rezi-t-i-ma T)ri konvektivnora te-Dloobilene).
PiMODIGAL: TeploenerGetika, 58, No.4, pp.79-60 (USSR).
ABSTRACT: Des-ite -'Gli~,~ practical i~--aportance of unstable thernal
convection, the problem has been noo-lected. A strict
Iihooretical solution presents Ereat mathematical
difficultie--. Therefore, use is usually uade of formulae
approDriate to the steady state; their ap-;-licability
to unstable conditions of heat exchanze is as--imed.
However, there is as yet no way of astimatinr! the error
inherent in this assumption. TI.-.e present article uses
aethod of succes~-.-.ive aDpro::i.-,, ].-,;ions to establish a
simple e-,-Dression whereby the applicability of the
ascumptio-n can be roughly calculated. Formulae are
derivee~ to determine the applicability of the steady
convection for.,imlae. They are :-,pplied in a numerical
Card 1/1 e----r-v-jDle on turbulent flov.- in a pipe, and the u-se of the
steoJy state equations is found to be admissable.
ASSCCIATION: All-Union Theriro-Technical Institute.
(Vseso,,,uzn3,-j Teploteldmiches-kiy Institut).
AVAID~BLE: Library of Congress.

31582
5/124/61/000/011/023/046
1~2 60, S-0 of) D2,77/D305
AUTHOR: Sidorovj_E?A.
TITLE: Radiant and convection heat exchange in absorbing
medium
PERIODICAL: Referativnyy zhurnal, Mekhanikap no. 11, 1961, 88,
abstract 11B591 (5b. vopr. teploobmena, M., AN SSSR,
1959, 49 - 52)
TEXT: In the energy equation of a flat laminar boundary layer of
a incompressible fluid the heat gain is assumed to be due to ra-
diation and influence of viscosity is neglected. Direction of the
radiant beam is considered to be normal to the streamlined surface
and U"he fluid is optically grey. The energy transfer equation is
taken in the form averaged over direction and on its integration
the approximation is assumed that inside the -boundary layer the
temperature is constant and equal to that of a free flow outside
the boundary layer. The resulting energy equation is
Card 1/3

Radiant and convection heat
3T 3T) eT + fmcTn2 4
Pc(U 57 -t- V57 aY2 (T1
S/1234~W12/000/011/023/046
D237/D305
4) -my
- T0 e
where u. v9 p. T are velocity components, density and temperature
of the fluidj A - coefficient of thermal conductivity, c - heat
capacity, T1, To - temperature of the surface and the fluid on the
boundary of the layer# F_ - coefficient of blac"kness (absorption)
of the surfacep 1- Stefan's constant, n - index of refraction of
fluid, m = 3/2 kt k = coefficient of absorption of fluid. This
equation is solved (to 1st approximation) by modified Shvetz me-
thod (Shvetz, VI.Ye. Prikl. matem. i mekhan. 1950, 14, no. 1)). The
solution is sought of the equation with the L.H.S. neglected, sa-
tisfying the condition of equal temperatures on the wall and on
the boundary of the layer, when the thickness of thermal boundary
layer 6 is the 2nd approximat-icn obtained by Shvetz method, when
radial heat transfer is neglected. Thusq the a-u.thor obtains the
following expression for heat iransfer intensity q through The
wall
Card 2/3

S/1 243/3-56812/000/011/023/046
Radiant and convection heat ... D237/1305
A(T 1 -T0) q, (1 ~_.6)
q = --s- I- M-F _ ,
q, - intensity of incident beam on the wall. For kt/a 0~-- 0.1, where
a0 - coefficient of heat transference# convective and radiant heat
transfer are practically additive and can be calculated separately.
[Abstractor's note: Complete traislationj.
CI-K

AeISZOO 68767
AUTHOR: Sidorovo Z. A. 3/170/59/002/11/013/024
B014 B014
TITLE. Calculation o~ Resistance and Convective
Heat ExchangeNUnder Turbulent Nonsteady
Conditions %
PERIODICAL: Inzhenerno-fizichookiy zhimnalo 1959s Vol 29-Nr-119~pp 86-91 (USSR)
ABSTRACT: Proceeding from the not o'.' equations (1) for heat transfer under
arbitrary conditions, the author derives equ%tions (5) and (6) for
quations are considered to be
equations (2) and (3). Thisse two
o;
sufficiently accurate solutions (1). For practical purposes#
however, they proved to bij not very useful. The author suggests
to derive less complicated and thus more useful approximate solutions.
A correction of the solut:.on for steady conditions leads to formu-
la (9) for nonst*ady cond:.tions, which has the form of the ordinary
Bernoulli differential equation. Next, formula (11) for the resis-
tance coefficient is deduned herefrom. A similar way is chosonfor
equation (6) for the heat exchange. Thus, formula (20) is obtained
which is used to compute Ithe Stanton number. There are 5 references,
4 of which are Soviet.
ASSOCIATION: Institut toplofiziki SO A.'T SSSR (Institute of Thermophysics 509
AS USSR)
Card 1/i

67604
.24.5-200 SOV/179-59-5-26/41
AUTHOR: Sidorov, E.A. (Moscow)
TITLE: The Interaction of Convection and Radiation in an
Absorbing Medium
PERIODICAL:lz-estiya Akademii nauk SSSR, Otdeleniye tekhnicheskikh
nauk, Mekhanika i mashi~aostroyeniye.. 1959, Nr 5.
PF 134-136 (USSR)
ABSTRACT: The paper is a continuation of previous worN (Ref 5).
The plane motion of an incompressible fluid?kith constant
physical properties nea,r a non--Lsothermal surface is
considered. The equations for the conservation of mass
and energy and for radiational transfer are written in
differential form, the latter equation involves the
Stefan.-Boltzmaxin consta-it and the refractive index of the
medium. These equations are solved by means of exponential
functions to obtain the radiation transfer, which is then
substituted in the energy equation. The resulting equation
is solved by%an iterative process for both turbulent and
laminar flow to obtain the final equation for total heat
transfer, There are 6 Soviet references, Lr
SUBMITTED: July 13, 1959
Card 1/1

AUTIHOR: Sidorov, S.A. (MOs cclif) Eu .8 1 Irl
tz,~i 11i Y dr ziu i
TITLE: The Inf lue ~(~,eoj~ Init tal Section
Rosistanco, raM~.rlcjj u
Aj
PERIODIC-AL-, Izvesttya Akademii nauk SSSR, Otoft~,Ienlyq
nauk, Flekhanika -4 Y-ashinostroypniya~ 19% NT
p 150 (USSR)
ABSTRACT: A-V-1,-empts ~-o esta-blist. ~,oretfe-l and
corrections allawing fol, the 'Lixfluenoe D.,' th--'
section r;f the tu'te Lave already
4
Bussinesq (Refs The rl,!~.,Zt
giving a b;A:5-1;.s fcr
calculation of hydral-lic r e s -*L,-; t a ndn tl-,e
section is the relatively rec-~n,,
8.14, Targ (Ref 4). The w3curacy, of tiie sAutic'n
established by the vexy good correspondev.~~;-, -wl.vli
experimental distribution of f'--c,w velocJ*y in T;ii~,-,e
by Nikuradze (Ref On th..; ba.,~js of S.M. Talr;,-s
Car,1 f indings, the fall -i-r. Pre 7- L-117-e P .CCOV"irevi the
Section Of entry (x =01 p
an a-i-bitrary secti.on diatan,:.a x Crom ',',rkp entrairi,;~i
C~Llcula-t'-.Pd from zhe chango alc,,,-;~7 t''Au .-)f +-,~-,be ~,-r

t a
The I r-., fl u e n cc ni t 1 n. 1 S 9 r; - L , ~T-% c, i--. I Va U
L-,~~,-ainEl- Flo-w of iz'~ Ali'jij:',
tl,,e ic--al. anr3 tlie mean hydraliIA",
-esistance O'M irtin-
the final -fesult can be wr-itten
cc;
dp el = 6 4 2 ~'.r
T exp
R Ud/
0
0 R J- Ok-
whi-re R is Reynold Is rxzber i U the mean f 10 v., -a I C, i tv
d thG equivalent diamete':- of 1.11.3 zube; and c,
-re.s.pectively the kicematin. vis~xjzi-',y creffi---4crIt and
/ '. .: 1 - '~
derisity of the novir.e, fluid; 'ind Of k r.
C-a r d successive roots Tj e-'-- the equat--"-~n i2 = 0 if ttle
s e -"-) nd t C. M,f e. fo rr,-, U la -2 ( i ) a I id a ruo I n -%. cc t.
the ~,~duF, of the firit, t9-"-,

s
CI
L.aminar Flow --~f 11 Tub- IL
L O~-, I R
A. oll
f o u nd ',:, r tiic
f
Y I if .4i tL ~e flRding-q of
ee T;P
1~
Velocity of tiv? iairial section, V, e
t'he
mean fric-IOL,~nal i3 2(~, largar ar,d
L"I C, t, ~'~ R
it~- 1*011ows from Eq ('+'/
so diat 4.n the I(Ia.,"ori'y
eq:uati,~r.
t n a IR
s ' r i r.. tly s p val i 6 only 1'o i
L 4,
vlien c) a.---d acrvrfc.~ion~- ~6 1~ "'41
VA of tLese Oull-I -[~m
lue s
for
-Lons thud; cbl:a I-rked -.C~ .w:i n- 1
E press C, o
C a r (-1 slow 0 :, "he C,-)-- - C- rid -I n s a r i e 1i FO T
reason the followi.rg -m-11FI~ alo
suggested for cal,2u.-Iating tne mr-,~.n hid:a,.Cl,~
0

The Infliience of Tm.t---:;-- otl
Lam Flow of L."t'U'lid j~n T-Aes
c r) e f f _i- c i- .n t
S 01i Z
JC
0 -30 x
X
Ea,Uations, f,;Ovey pruct,-Cally ali t!le
the par-amozer Rrllx 0 tc 1000, in l-'aXImuir,
ery-Or or approxiLnv-fou dr,e:: nc'; 3%, P~)r
we give tile result's Of cal CuLat; -icIr"5 fo:. -i..rl e
Ca r d
a,,rallablp. forrmiae iind 0-!3c, by fQ
ReynoLdis number.-I
Rd/-x. 10 -'0 ~C, i0o ~100 NCO

The S-
Laminam- F I c-) w f Liqu.,L-~'S I'Ti 'N
C-

R~~- -5

1 Sn, I I t- L EL1, J d
PT-,,~ ?n7t 3TT'a ta
J.
Vol. L , I L 1,-,i
p rand tA" L. Ti.tletn-~. 1). lip'-0- 3 -a a .
2, ODT1,
_T Basi,7 py3blem-s
2L
C.a.,- d ~~i
F. N 1'
It is -LS 'A -ccmp.-Let- translfi*
SU 31,,' IT TED: -P., -10,79

10W
-AUTHORs Sidorov, E.A.
SOV/170-59-6-18/20
TITLE: On the Calculation of Hydraulic Resistance in the Initial Section
of Pipes Under Turbulent Conditions
PERIODICALi Inzhenerno-fizicheskiy zhurnaL, 1959, Nr 6, PP 111-115 (USSR)
ABSTRACT: In order to investigate the effect of the initial section of a pipe
on hydraulic resistance, the author writes down equations of mass
and moment conservation in dimensionless form. He makes use of the
results of two experimental findings: 1. One of them expresses the
law of velocity distribution over the cross section of a boundary
layur, and 2. The second is the statement that the character of
development of a boundary layer in the initial section of a pipe
is similar to the character of development of a boundary layer,
-when a liquid flows around flat surfaces. The boundary conditions
are obtained for the distribu,;ion of surface tension, af, and the
coefficient of hydraulic resiotance along the length of a pipe 9 9
and the problem is reduced to a system of six algebraic equations.
Card 1/2 The solution of this system y--elds the expressions for average

SOV/1,10-59-6-16/20
On the Calculation of Hydraulic Resi.-itance in the Initial Section of Pipes Under
Turbulent Conditions
hydraulic resistance, Formulae 15 and 16, and the values of relative
coefficient of hydraul--c resistance, plotted versus the values of
pipe length, are shown in Figure 1.
There are: 1 graph, 1 table and 11 references, 10 of which are
Soviet and 1 German.
ASSOCIATION: Energeticheskiy institut AN SSSR (Power Engineering Institute of
the AS USSR), Moscow.
Card 2/2

69942
S/024/59/000/06/023/028
E032014
AUTHOR: Sidoroj-, E. A. (Moscow)
TITLE-~ Generalization o-f the Grets Solution to the Case of
Radiative Heat Transfer-oO
r
PERIODICAL, Izvestiya Akademi.i nauk SSSR, Otdeleniye
tekhnicheskikh nauk, Enere;etika i avtomatika, 1959,
Nr 6, pp 183-185 (WMR)
ABSTRACT: Grets (Ref 1) has given a solution of the problem of
convective~heat transfer in the case of laminar flow
of liquidsTin stabilized sections of tub Lz6 The
differential equati3n for the heat transfer, which does
not take into account radiative terms, is given by
Eq (1), where T(r, z) is the absolute temperature of
the liquid, r and z are the radial and axial
cylindrical coordinates, a is the reduced thermal
conductivity (i.e. the ra-,io of the thermal conductivity
and the product of the specific heat and the density of
the medium), and ir(r) is the velocity of the liquid.
Grets has found solutions of Eq (1) for two cases,
namely. when the volocity distribution is parabolic
(Eq (2)), and when it is .-onstant (Eq (3)), However,
Cal',l 114 it can be shown (R,,-f 2) t:iat provided the condition

69942
S/024/59/000/06/023/028
E032/E214
Generalization of the Grets Solution to the Case of Radiative
Heat Transfer
2RP/z e, 15 is satisfied (and it is satisfied in many
practical cases), tte two solutions are almost identical.
In this condition 11 = 2UR/a. The present author assumes
that this condition is satisfied and writes down the
energy equation in the form given by Eq (5), in which
radiation effects a--' e included in the form of the second
term on the right-hand side o` Eq (5). In this
equation, p, c and X are the density, specific heat
and thermal conductivity of the liquid, k = 3a/2, and
T is defined by the fourth equation on p 184 in which
D = 2R is the diameter of the tube, a is Stefan's
constant, and n is the refractive index. Eq (5) is
then linearized using the substitution given by Eq (6),
where Tm is given by Eq (7) and To and Tj are the
temDeratures of thE liquid at -r;he input and of the walls
of ihe tube respectively, The equations are then trans-
formed into a dimensionless system of coordinates, which
is defined by the relations immediately above Eq (8). When
Card 2/4 this substitution is carried out, the heat transfer I --"

69942
Generalization of the Grets Solution
Heat Transfer
Card
S/024/59/000/06/023/028
E032/E214
i;o the Case of Radiative
equation can be revn-itten in the form of Eq (8), the
boundary conditions being
e = 0 when x - 0
9 finite when y - 0
0 = 1 when y = 1
The temperature distribution is then given by the last
equation on p 184 in which JO) Jl and I are the
ordinary and modified cylinder functions and Pi are
the roots of the equation JO(x) - 0. F;r a transparent
medium (B tending to zero), when the radiation can be
neglected, one obta:Lns the solution given by E (11) which
is the same as that obtained by Grets for pure?y convective
heat transfer. The total heat flux (I passing through
the walls of the tube (per unit area) can be found from
Eq (11) and is given by Eq (12). An important consequence
of EqS (10) and (12'i is the fact that when radiative
corrections are brought in, the temperature drop and the
quantity of heat gii-en up by the medium change more i b.""

699h2
S/024/59/000/06/023/028
E032/E214
Generalization of the Grets Solution to the Case of Radiative
Heat Transfer
rapidly along the length of the tube as compared with
the case when the correction is not included. There
are 4 references, 3 of which are Soviet and I English.
SUBMITTED.- June 2, 1959
Card 4/4

SIDOROV.. B.A. (IIoiskva)
Calculating the temperature dependence of the heat comiuction
coefficient in nonotationary conduc*dve heat exchange.
PM no.4:62-63 11-D 960. (MIRA 34:7)
(Haab-40a6mme 1)
ii,

S/170J60/003/005/012/017
B012/BO56
AUTHOR: Sidorov, E. A.
TITLE: Calculation of the Combined Heat Interaction Between Solid
and LiQuid4Medi&
PERIODICAL: Inzhenerno-fiziehaskiy zhur-ial, 1960g Vol. 3, Ko- 5,
pp. 106-110 1%V6
TEXT: Approximation methods for the calculation of non-steady heat exohangt
are given. The problem to be solved is tht following: An opalu-9-1-5111rWor-
arbitrary shapep round which a liquid (or gas) flows, and which has the
absolute surface temperature T, the integ7al degree of blackness F_ and the
heat-transfer coefficient a is assumed. V is the velocity and T the
absolute temperature of the thermally not disturbed part of the liquid
flow. q is the density of the beat flux due to radiation from outside
(upon thi surface of the solid). As a retult of the compli-zated heat ex-
changep the resulting heat flux q, PaSBSE through the unit of the body
surface. It is assumed that the thsrmoph~sical properties of the liquid
(or gas, respectively) and of the solid io not depend on temperature. The
Card 1/3

Calculation of the Combined Heat Interaction 3/17 60/003/005/012/017
Between Solid and Liquid Media B012YB056
functional interrelation between V, T 0 , qoj T19 and q, is sought. First,
the heating of the body by radiation without convection is investigated. In
this case, only the interrelation betmeen q 0, T1 and q, need be found.
The formula (1) for thermal conductivity is written down, and it is shown
that consideration of heat transfer by radiation leads to the nonlinear
boundary condition (5). As a concrete example, the heating of a plane,
rather thick wall by radiation is investigated. The thickness of the wall
makes it DOssible to regard it as a gemi-limited body during the time of
investigation. If internal sources for heat production should be lacking,
the differential equation (6) may be written down, for which the boundary
conditions (7), (8), and (9) are given. Assuming formula (13) the boundary
condition (8) is linearized, and formulas (17), (18), (19), and (20), which
determine the required interrelation between q 0, T1,and q,, are derived.
Next, the convective heat exchange 13 investigated in consideration of
radiation. For this case, the approx~-mate formula (24) is recommended,
where the nonlinear boundary condition ~5~ becomes formula (25)- In the
present case, the solution of equation 1 makes it possible to determine
the interrelation between q,, T19 qos and T*. a - a(V) is agsumed to be
0
Card 2/3

Calculation of the Combined Heat Interaction S/170/60/003/005/012/017
Between Solid and Liquid Media B012/BO56
known. In conclusion, the flow round a body of a great transverse thickness
is investigatod as an example. In this case, the body may be looked upon
as a plane wall of unbounded thickness. There are 5 references: 4 Soviet
and 1 British. /C-
ASSOCIATION: Institut teplofiziki SO AN SSSR
(Institute of Heat Ph.79ics of the SO AS USSR)
Card 3/3

10. IIiUOO
Ik, J j
s ov/6 9 -8 - 3
-12/32
AUTHOR:
TITLE,: Choicu of' Coolant Cur fluclt--ai- R,-~actors. Letter to the
E di t o r
P ERI 0 DI CA 1, 1 Atomnaya enurj~-.Iya, 1950, Vol 8, Nr 3, pp 252-2511 (USSR)
A13STRACT: The author ant.lyzed variOLIO 4.,oolants frorn the standpoint
of heat-tran.-A*er arid energy ised in transporting the
mater-tal. Th(! goal was to br-Ing the existing data by
Qoodniall Up to date by using more recent information by
Vargaftlic (TeploftzichezIciye svoystva. veshchestv,
Spravochnik (Thermal Properties of Materials Manual)
edited by Var1r,aft1k, M., Go-,,energoizdat, 1956) and
Mikheyev (Osnovy teploperedeci-ii (Introduction to Ifeat-
Transf(-Ir) M., Gosenergoizdat, 1956). To compute the
heat-transfer coefficients oT heat carriers of the first
class (liquids arid gases with the Prandtl number Pr >
the author used the eqUatiOll valid for the stabilized
turbulent floas
Card 1/1~

Choice of Coolant for Nuclear Reactoro.
Letter to the Editor
0,023C). V-11.8
78327
SOV/89-8-3-12/32
(1)
where G depend3 on the construction of the heat ex-
changer, and ~, and i) are coefficients of heat conduc-
tion and kinematic viscosity.. respectively. For the
second class oC carriers, representing liquid metals
(Pr = 10-2 to LO-4 ), the author uses the approximate
equation:
P)
Table 1 contains the result of the comDutations. The
author also deyelop:3 an expression for the dimensionless
economic coefficient of heat-transfer which is equal to
Card 2_/~ the ratio of the heat energy transferred by a particular

Ch0i(-'C Of COOli-1111- f0l' NUCIC.Al- R0a(AU11:,.
Lc.,tter to the EdItat, SOV/89-8-3-12/32
Table 1. fleat-transfer coeffl.clelit.; for 1,ariou3 heat carriers , (a)
heat carrigr;,(b) heat-tran2fer coefficient (relative unit--2.8
kcal-secO- /m'-h-deg) at temperatures in `C; (c) air; ~d) carbon diox-
Ide;je) water, vapor (Oil OatUl'atiOl-I CUT~VU); (f) water on SatUration
curv ; (g) dowtherm (11(juld b1phenyl mix-,ure); (h) saltpeter mixture
melted oalt (i) Inercury; (j alloy (25% Na + ~5%iK);((k) soditun;
alloy. Bi + 11'3.r)% Pb~; (m). llthiufn; 11 t n; o) U2111LIth.
5u0
Card 3/5
(CI 0,7 0,7
at-) . . . . . 1, 1,0
1.41 lip 7o -
1,11. 1#)- 1.:!. lip I. lip,
- - lip, -,-, Io 1 2.5. it 102
- 2,:1-11)" 3.01101 .1,3- 11P 3, 2. lot
. . . . . . I , 2. - 10 13 1 :1. IW I :I. Ito -
8,9- 102 8 "21 - I o *3 7,9,1114 7,:I.jl)l 7,0,102
. . . . . . - 1 3. 140
3 1 1-1 -110
ll 1 , 2. 103 1 , I . I t)3
. I . 1, 1.111 1, I-Io 1.0. 1113 1.1-103
1 . . I . I I h - IlP I, H. 103 1,8.1(p
. . . . . . . . . . . . 1,1;. lip 1,5- lip
. . . . . . I , I - 110 I'l. 11)3 1,2-103

chojt~e or cooiant for Nuclear 7832
Letter, to the Editor SOV/~ 9-8-3-12/32
SUBMITTED:
coolant to the mechanical energy needed for its transport
through tubes. Computed results are tabulated in Table
2. The final choice of coolant should, of course, also
take Into account other technical and economic factors,
e.g., corrosion effects, stability) etc. There are 2
tables; and 4 references, 3 Soviet, I U.S. The U.S.
reference is: Scientific and Technical Foundations of
Nuclear Power Production, C. Goodman (ed.), M., Izd-vo
inostr. lit., 1948-1950, Vol 1, p 287; Vol 2, p 124.
December 18, 1958
4/5

r "o
(!,Irvier ; (b) economic
O-Aa tlve uni t-113 1,,cal , see
1 0") o.1
a q), r-:0, 0
; wt~ Ln
C); (c
to 0)

0.3i
11,37 11.41

11.31

74)

SIDOROT. B.A.
Bffect of internal beat sources on convective host transfer.
Atom.energ. 9 no-1:51-52 J1 16o. (MIR& 13:7)
(Heat-Trarismission) (Heat-Convection)

SII)*Ov, E.A., inzh.
- -111~411
PreciBe calculation of themial insulation. Teploenergetika
8 no.3:88-439 Mr 161. (MM& 14:9)
(Insulation (Hoat))

S/17q/t;3/oo6/O02/O18/018
BIOB/B'le6

AUTHOR: Sidorov, E. A,
TITLE: The critical diameter of a spherical heat insulator
PERIODICAL: Inzhenerno-fizichetikiy zhurnal, v .6, no. 2, 1963, 131-132
TEXT. The critical diameter, i.e. that diameter at which the heat
resistivity has,a minimum, is calculated for a spherical heat insulator$'
the dependence of the coefficient a (x) of convective heat transfer on
x
the diameter of the sphere being taken into consideration. x - D/d is
the ratio of the variable-outer diameter D afthe inaulation to the
constant inner diameter d. The heat resistance of & spherical body in
x2 n
r - r + r(I - 1/x)/2k + 1/a d The' relation Nu - ARe was-found VK
0 nd x
experimentalfy for convective beat transfer'(B. D. Kantselloont
-
F. A. Timofeyeva. Trudy Tsentrallnogo kotloturbinro~o instituta
(Proceedings of the Central Bo~bler and Turbine Institute), v. 12, no.
Yashgiz, 1949). n . 0 and A . 2 for Re