SCIENTIFIC ABSTRACT KATILYUS, R.V.[KATILIUS, R.] - KATINAS, V.YA.

• Document Type: CREST
• Collection: Scientific Abstracts
• Document Number (FOIA) /ESDN (CREST): CIA-RDP86-00513R000721120003-5
• Release Decision: RIF
• Original Classification: S
• Document Page Count: 100
• Document Creation Date: November 2, 2016
• Document Release Date: June 13, 2000
• Sequence Number: 3
• Publication Date: December 31, 1967
• Content Type: SCIENTIFIC ABSTRACT

KATILYUSY R. V.[Xatilius, R.]; VANAGAS, V. V.[Vanagaa, V.]
On the antipy=etrization of the function of equivalent electrons.
Idet ak darbai B no.10-22 161. (EUI .10: 9)
1. Institut fiziki i matematiki Akademii nauk Idtovskoy SSR i
VilInyusskiy gosudaretvenny7 universitet im. V. Kapaukasa.
(Electrons) (MAtrices) (Functions)

T -1 N- - -
7777--t,~,
iskoy SSR. Vil'nyus
InatitUto Of PhN'SICS and natheratiCS, AN LltSSR)
ll--,T-:~~--,., "J 7

-KATILYIUS,), R. [Katilius,R. j
Scattering on the central Potential in a high magnetic field.
Fiz. tver. tela 6 no.9:2837-2845 S 164.
(MIPA 17:11)
1. Institut poluprovocinikov AN SSSR, Leningrad i Institut fiziki
i matemati.ki AN Litovskoy SSR, VilInyus.

1. KATIN, A.; TIGANOV, G.
2. USSR (600)
4. Cranks and Crankshafts
7. New method for testing the parallelism of the axes of crankspins and crankshafts on
the spot, Engs. A. Katin, G. Tiganov, Yor.flot. 13 no. 4, 1953.
9. Monthl List of Russian Accessions, Library of Congress, APRIL 1953, Uncl.

VOLKOV, Vasilly Alaksandrovich; YIJRJI,IOV, Ivan ZakhtwovIch;
A.F., retsenzent; KUPTSOVA, L.D., rOALIE'lizent; 'SCM M,
4"~'~-':Ip"'OFdtsenzentj RAZa"OVSKAYA, Ye.V.p red.
[Technolog of leather] Tek-hnologlia kozhi. Moskva, Leg-
kaia industrilap 1964. 429 p. (1-1111A .18:2)

KATINq A.I.
Container tilter and multifork gripping deities of motor loaders
for loading piece freight on ships. 8iul.tekh.-ekon,inform.Gos.-
nauch.i tekh.inform, no.11:84-85 162. (~aRA 15t11)
(Fork lift trucka)

K-t,TP11, 11. V.
Katin, A. V.
"LiT) cancer and its treatornt with rgdon and radioactive cobalt
(Clinical-r*orpholog,ical investii-ation)." Central Sci hes Roent-
,-cnolo,,-icI-l vaid Radiological Inst, Kin Pealth USSR. Lonim- i Ind) 1'Lt,,
(Dissertation f or to degrcc of Doctor 'Ln Ecdical Science)
Knizhna,,,a iCtOJ~JLS
No. 1-'., 1956w Moscow

DANILOY, Sergey Semenovich;-XATIN, Isaak Iosifovich; IWICKKOV, V.I.,
spetsred.; FRISHHAN,'Z-S,,-ro'd.izd'-Va; IROZHZHIRA, L.P.,
tekhn.red,
[Utilizing the curves on preliminary drawings for ship
handlingj IspolIzovanie krivykh teoroticheakogo chartezha
v audovykh unloviiakh. Leningrad, Isd-vo "Horskoi transport? It
1959. 39 P. (HIRA 13:2)
(Shipbuilding) (Ship handling)

KATnr
Effect of the diameter and shape of drill bits on the coarseness
of cuttings c1rilling holes by pneumatic perforstors. Izv~vys.ucheb.
zav.; geol. i razv. 1 no-5:116-120 my '58- MIU 12:2)
1. Moskovakiy geologorazvedochW inatitut imeni S. Ordrhonikidze,
kafedra gornogo dela,
(Boring machinery) (Borings)

ID.TIN, X.P.
Studying the effect of weight on bit on drilling rates. Trudy
MGRI 34:55-62 159. (MIRA 13-12)
(Boring)

KATIN, K.P.
Possibility of developing the drilling of blastholes and
wells with annular bits. Izv. vys. ucheb. zav.; geol. i razv.
no.12:140-144 059, (MIRA 14:6)-.
1. M65kovskiy gkologorazvedochnyy institut imeni S.Ordzhonikidze.
(Prospecting) (Boring-Eqvipment and supplies)

KATIN, K. P., Cand Tech Sci -- (diss) "Percussion boring of bore holes
L
by circular boring bits (from experience in prospecting work).-' I'-105cow,
1960. 24 pp with illustrations; (Ministry of Higher and Secondary
ialist Education RSFSR, Moscow Geological ProspectinE Inst im. S. Ora-
zhonikidze); 220 copies; price not given; (KL, 28-60, 160)

KATIN K P
Dr4114n holes with core bits. Razved. i okh. nedr 26 no.6:25-29
Je 160. - NIRA 3 5:7)
1. Moskavokiy geologoramdochnyy institut.
(Boring)

RODIONOV, N.S.; KATIN, X.P.
Using blastholes of various diameter in workings of small cross
sections. Izv. v7s. uchebe zav.; geol. i razv. 7 no.7:119-121
Jl 164 (MIRA 18.62)
1. Institut gornogo dels. AN SSSR im. Skc,-hinskogo i Wesoni"y
nauchno-issledovateltakiy institut toratnykh metallov~ Ustl-
Kamenogorsk.

VESELOVSKIY, Aleksandr I'P ?..ev Rikolayevich;
KONYUSMJKG, I.A., r, 4. 1. . red., SORKIN,
M.Z.9 tekhn. red.
[Radio-controlleu "i:ap ~'~4i"'i..)upravliaemaia modelt
korablia. Moskva, Izd-vo DOSAAF, 1963. 80 (P&A 16:10)
(Ship models--Radio control)

;4:
il. !:~
STOLPXR, M.B., insh.; KATIN. N.P.. insh.-, BRODTAMKIT, T.M., kands tekhn. nauk,
Answers to readeres KieloroiL 10 no,5:44-45 157. (MIRA 1l,-4)
(Gases)

KATIN, N.I., inzh,
Testing the creep of concrete subjected to high working stresses.
Trudy NIIZHB no.4:74-153 '59. (mm 12:9)
(Concrete--Testing) (Straina and stresses)

KATIN, N. I., Cand Tech Sci -- (diss) IlExperimentnl investigation
of creep in concrete at high stresses." Moscow, 1960. 24 pp, with
graphs; (Academy of Con2truction and Architecture USSR, Scientific
Research Inst of Concrete and Reinforced Concrete NIIZhB); 150 copies;
price not given; (KL, 18-60, 151)

HATSELIKSKIY
.. R.N.', kand.tekhnneukt KATIN, kavd*tekhn6nmuk;
STULIGHIKOV2 A.N.p inzh.
Long-open reinforced concrete ribbed arch. Promatroi, 40 no,112
3le-36 162,, (Arches) (Roofing, Goncrete) (MM 15:12)

KATIN, V.
Africa looks tonxd the future. Vnesh. torg. 42 no-11:32-34
162. - -7 (MIRA 15:11)
(Afrieg~ blitics)
(Afrioa-Economic conditions)

KOVALEV., N.G.; ZMEYEV, A.A.; LUKIN, Ye.l.- FADINA, G.I.; KATIN.L
y
V.K..X-LYSHCHIKOV, YU.T.; VLASOV, A.V.; KARFOV, I.H.;
IrTVH-Ovp A.S.; DAJUNYAN, M., red.; MOSKVINA, R., tekhn.
red.
(Africa in figures; a statistical manual) Afrika v tsif-
rakh; st4 isticheskii spravochnik. Moskva, Sotsekgiz,
1963. 5 1 p. (MIRA 16:11)
(Africa-Statistics)

KATIN _Vladimir Konstantinovich; SHMSKAYA, V.A.9 red. izd-va; PAVLOVSKIYI
A.A,p Wicums reae
[telumon; economy and foreign trade) Livau; ekonomika i vneshniaia
torgovIia. Moskvat Vneebt6rgizdatt 1961. 3~P.5 p. (Mu 14-9)
(Lebarion-Econondo conditiona) (LebWn-Comwree) -
I

KATIN.,j,jad~w1r-, Kona tantinovich,' -.LAVRENT IYOVit, Ye.V., red.;
--- ---- SHAPOVALOVA, N.S., ml-adshiy red.; ARDAWOVA, N.P.j,
tekhn. red.
[In Tunisia; travels and adventures] V Tunise; puteshestviia
i prikliucheniia. Moskvap Geografgizp 1963. 9~ p.
(MIRA 17:3)

,..-KATINP V.
- -kV
Strengthening the economV of Tunisia. Vneshetorg. 42 no.7:20-2.1
162, (MM 15:7)
(Tunisia-Economic conditions) (Russia--Cn rce--Tunisia)
(Tunisia-Co=erce--Russia)

SOV/147-59-2-2/20
AUTHOR: Katin, Ye.I.

TITLEs Spreading of an Incompressible Turbulent Stream
over the Surface of a Circular Cone (Rasprostraneniye
turbulentnoy strui neszhimayemoy zhidkosti po
poverkhnosti konusa)
PERIODICAL; Izvestiya vyssbikh uchebnykh zavedeniy, Aviatsioxxnaya
tekhnika, 1959, Nr 2, pp 12-20 (USSR)
ABSTRACT: Knowledge of the flow parameters of a gas jet issuing
from a circular nozzle and flowing over a conizal
surface Is essential for solving many practical
problems. The case of the laminar viscous flow with
a swirl is considered in Ref 1. This solution appears
applicable also to the case of the turbulent flow if
the coefficient of 'teddy viscosity" be assumed constant.
In the velatity profile so obtained the maximum of the
fundamental. component occurs at a distance from the
cone surface equal to 1/4 of the thickness of the
stream tubc. This is only an approximate solution.
Exper-Imentv show that this maximum Is appreclably
Card 1/6 nearer the surface. However, from the analysis of the

SOV/147-59-2-2/20
Spreading of an Incompressible Turbulent Stream over the
Surface of a Circular Cone
experimental data it may be concluded that friction
affects the velocity distribution only in a
relatively thin layer close to the surface and its
influence is quite insignificant on the flow
parameters further away from the surface. Consequentlys
'when the knowledge of the flow parameters only is of an
interest,not the effect of the flow on the cone,
surface friction may be neglected altogether. This
assumption is made in this article and, as shown in
Fig I only the axi-symmetrical flows are considered.
The distance t between the cone apex and the orifice
is assumed sufficiently small so as to ensure the
uniformity of the free stream before it impinges on
the cone. With u and v being the mean velocities
In the x- and y-directions and T being the
turbulent shear stress, as expressed by Eq (3) in
which c is a constanto the momentum and the
continuity requirements lead to Eq (1) and (2)
respectively. Assuming now that a distance from the
Card 2/6 pole the flow is self-similar and that no friction

sov/147-59-2-2/20
Spreading of an Incompressible Turbulent Stream over the
Surface of a Circular Cone
exists at the surface of the zone, then as shown
in Ref 1, the equation of motion transforms into
Eq (4) and (5) where a is a constant of the
turbulence and um is a fictitious maximum velocity
of the flow (which would actually exist if no
friction at the surface were present), this velocity
being called the axial velocity. To solve the
problem fully its value must be known. It can be
found from the momentum prinuiple as given by Eq (6)
by considering the mass flow per second; u. is the
discharge velocity at the nozzle. Using now the
geometrical relations of the flow as shown in Eq (7)
and continuing this with Eq (5) and (6). the axial
velocity um may be found, Eq (8). By Eq (4)~ (5) and
(8) it follows that the dimensionless velocity
profile remains unchanged for a given cone angle a
but changes when a is altered. Thus when a = 09
Card 3/6 Eq (9) is obtained. In Ref 2 the corresponding

SOV/147-59-2-2/20
Spreading of an Incompressible Turbulent Stream over the
Surface of a Circular Cone
velocity for the case of a free jet is given by
Eq (10). Relating these two leads to Eq (11).
To analyse the validity of this similarity, t he
graph of Fig 2 is drawn. In this diagram a =-l
and al is obtained from Eq (11) and the full line
represents tha..solution of Eq (4). Vhen a = 900
(Fig 3), Eq (1:2) is obtained by substitutions of
Eq (13). This may be transformed to agree exactly
with the corresponding expression obtained in
Ref 3, from which Eq (14) follows. (In Ref 3 the
constAnt--war erroneously quoted as 1.46, it should
be %f1-.46 = 1.21) Some experiments were carried out
to test these relations. The apparatus is shown in
Fig 4. The flow was produced by a -wind tunnel with
exchangeable nozzles (1) of diameters 30 and 40 mm;
the cones (2) had 210, 30 and 406 at the vertex and
were fixed by the attachment (3) so that they could
be moved axially. Pressures were measured by the
Pitot tubes (4) held in the clamp (5) which 6nabled
Card 4/6 measurements of the x- and y-cuordinates. Fig 5 shows

SOV/147-59-2-2/20
Spreading of an Incompressible Tuxbulent Stream over the
Surface of a Circular Cone
the graphs of the total pressure and Fig 6 of the
static pressure for the discharge velocity
UO = 20 m1sec, nozzle radius r,, = 20 julm and the
semi-vertical angle of the cone a. ~ 20'. Fig 7
gives the velocity profiles for this case. The
graph includes also the theoretical values of the
axial velocity (0 points) derived from Eq (8).
The agreement is perfect. Fig 8 and 9 give the
dimensionless velocity profilesi this was obtained
by taking the ratio of the experimental values of u
and the theoretical value of um. The univeraal
character of the profile is clearly visible. The
full lines in these graphs represent the theoretical
relation for the case when a = 0.07. Since Eq
cannot be checked directly by an experiment, the
graphs of Fig (10)and (11) were drawn for this
purpose; these represent u =-f(x) for const.
In this case the velocity u ia directly
Card 5/6 proportional to the axial velocity, which can be

SOV/147-59-2-2/20
Spreading of an Incompressible Turbulent Stream over the
Surface of a Circular Cone
determined from Eq The graphs show that for
x >>180 mm the experimental and theoretical values
agree very well but for x