SCIENTIFIC ABSTRACT DUBOSSARSKIY, M.I. - DUBOV, E.YE.

• Document Type: CREST
• Collection: Scientific Abstracts
• Document Number (FOIA) /ESDN (CREST): CIA-RDP86-00513R000411330003-6
• Release Decision: RIF
• Original Classification: S
• Document Page Count: 100
• Document Creation Date: November 2, 2016
• Document Release Date: August 23, 2000
• Sequence Number: 3
• Publication Date: December 31, 1967
• Content Type: SCIENTIFIC ABSTRACT

DUBOSSARS11Y. N.1.1 DISFOMYM, Ye.ye.
- _.
Multiposition attachment used for grinding five-edged reamers,
StAn.i instr. 28 no.9:42 S 157. (MIRA 10:10)
(Grinding machines--Attachments) (Reamers)

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GIIEVUSIIEV, M.A.; KRASOV., L.N.; DUBOTOV'KQ,-Yu.V.; DIYAKOVA, N.I.
Color of Yakutian diamonds. Trudy IAFAN SSSR. Ser.geol.
no.6:87-96 161. (MIRA 14* 9)
(Yakutia--Diamonds)

BIXTKHKLN, IA.; WBOV, A., redaktor; TRUEBANOTA. A., tekbuicheekiy re-
d&ktoro------"""-"'
[Technical progress in the Soviet Union] Takhaicheskii progress v
Sovetskou Zoiuss. Minsk, 1954. 34 p. (MLRA 8:2)
1. Doystviteltuyy ohlen Obahchestva po rasprostrananiyu politicheskikh
I wachnykb snauly Belomaskoy 83R.
(Technology)

'GORYAOMN. V#G*; ~~- B 030-~,, -
Shear stress limit for several tn*s of White Russian peat.
Trudy Inst. torf. AN BSSR 6:365-372 157. (KRA 11:7)
'(Peat-Testirg)

-P U 00 vi // . 5.
KALININ, S.M.; LUPINOVICH, I.S.; P0100CHKO, I.S.; ABRAHChIX. A.P.; ALEMYST,
Ys.K.; ALISKIK, P.I.; AHBR'OSOV, A.L.; AUIREYEVA, N.K.; ANOXHIM. A.N.;
AFORIN, H.I.-, BABOSOV, H.H.; BALOBIN,V.N.; BARAI(OV.SKIY. A.K.-, Bsz-
DXNKO. T.T;; BILIGUY, B.3.; BOBKOVA, A.?.; BOLIMMOVA, V.P.; BUL-
GUOV, R.P.; VAGIN, A.T.; BILIDYLUSH, R.T.; VILIC.HINSKIY, A.D.;
VLASOVA, X.S.; VO=O, D,I.-. VOLUMV, A.G.; GABYSIM, K.F. [deceased);
GATKO, A.A.; GALASH3V, M,A.; GOREGLYAD, Kh.S.; GARKUMIA, X.P.; GOSTI-
LOVSKAYA, M.N.; GWBUNOVA, N.H.; GORSKIY, N.A.; GORFIRMI, Z.2i.;
GRUBIMO. M.P.; GUSAKOV, V.A.; GUDATKIN. A.I.,- DANILOVICH, A.F.;
D34MiT'YlV, V.A.; DRUIS07. Z.N.; DOROZMIN, N.A.; MOT,.-A.D.; DUBCV~
SKIY, Ta.K.; YNVTIKHIYri, B.Ys.; ZHARIKOV, I.S.; ZHILIN. A.?.; ZlfCUW.-
R071CH, A.M.; Z=UVEL1,3.H.; ZABELLO, D.A.; ZAKHARENK0, G.D.; Zu-
BETS, VA.; ITITSKIT, A.I.; KAGHMO, I.K.; KHDROV-ZIKHHAM, O.K.; KIDA-
LINSKIY, V.A.; KIMiYARLITS, A.F.-, KOVALEVSKIY, G.T.; KOVALICHUX, P.P.;
KOZHANOV K.Ya.; KOZWYSKIY, I.Te.; XOCHRTOVA, Z.H.; KIUVODUBSKIY.
Isp.; il~A7TAYT5XV. S.F.; XUSTOVA. A.I.; LAPPO. A.I.; LARIMHKO, Y.B.;
LASMVICH, G.I.; KALICIRWMIY, V.I.; KAUIKO, H.F.; KARKOVETS. A.F.;
YATSIM9,R.Ts.; HEDY=V, A.G.; KELITM, Ta.D.; KOISMY, I.G.;
KUSORDr, f.Y.; KUKHIN. N.D.; HAGORSKAYA, Ta.D.; NALIBOTGKIY, S.B.;
NIKCLAUVA, Yu.M.; HEDCLUGOV, I.T.; CRLOVSKIT. 1.A.; ORLOVSKIT. K.P.;
PANWIMI, A.A.; PXSKIN, A.L.; PROKOPOV. P.Te.; PUSHUTMV, I.I.:
RAZMYSLOVICH, I.R.-, RAZUK311KO, A.V.; RM13VA, Z.I.; RINKIS, V.A.;
ROVDO, A.I.; ROGOVOY, P.P.; ROZENBLTUM. B.X.; RTMDWOV, A.G.; RUSI-
NOV, A.A.; SAVCHSHKO, A.I.; SAPUROV, V.A.; SAFRONOV, I.P.; SVIRSKIY,
U.N.; OWAMRNNV, vops-0 WGEYXV, I.Ye; SM01OV, A,L,; SIDORENKO, G.M.1
(Continitad on next card)

KALININo S.N.---(continued) Card 2.
SKOROPANOV, S.G.; SIMUNICIMIKO. L.A.; SMIRNOV, T.Ye.; VTAROVffTOV,
K.T. (deceased]: W!RMOV, X.G.; SUSLOV, V.P.; SMORTNOT, G.Te.;
SMAROV, A.Te.; TIMOSHININ, V.D.; TISHLEVICH, I.I.; TROPASINO,
I.N.; TRIZ110. U.I.; TRIKA, N.K.; TUZOVA, R.T.; TTRNSKIT, R.L.;
UMAIISKIY. N.M.; URIYEV, T.M.; KHOTIKO. A.I.; KELOBOSTOV, S.N.-, TSZ-
MWOVICH, F.V.-, CHYJWAVSKIY, 1.0.; CH=OVA, Ye.l.; CMOSOV, U.N.;
UUMM's V.I.; SHIKHALJMV, N.Y.; SMYAR, A.Ye.; SHCHERBOV, N.A.;
YURGMIS, B.A.; TMOMS, M.K.; TAKOVL-T-,'T, B.I.; TAKOLSON, S.A.; TARO-
GOVICH, A.A.; LUTSMIKO, H.U., red.; LARIN, V., red.; KALECHITS, G.,
takhn.red.
(Measures for Increasing agricultural production per 100 hectares of
land on collective and stnta farms of White RunaisJ Heroprilatlia p0
uvelicheniiu proisvodstva sel'skokhosisistvannoi produktaii as 100
gaktarov semellnykh ugodii v kolkhozakh i sovkhozakh BSSR. Red.kolle-
giis; I.S.Lapinovich I dr. Minsk. Gos.izd-vo BSO. Red.sel*khos.
lit-ry, 1959. 601 p. (MIRA 13:4)
1. White Russia. Kinisterstvo sallskogo khozynystva.
(White Russia--Agriculture)

NABATOVA, K.A.; DYMSHITS, VINDGRADOTA, V.P.
Shot peening the transmission gears of the Moskvich antonobile.
Ayt. i trakt. prom. nn.6:29-31 J3 156. (KLRA gig)
1. Nauchno-looledoyatolOokty'avtomotoriVy Institut I Moskovskly
zavod malolitrashnfth aytomotiley.
(Automobiles--Transmission devices) (Shot peening)

1. PCM0IITKTYj A. A.; DUBOV, A. GA
2. USSR (600)
4. Measuring instruments
7. Measuring apparatus for demonstration. Fiz. v shkole 12 no.6 1952.
9. Monthly List of Russian Accessions, Library of Congress, February .1953. Unclassified.

DU-~W, it. G.
DU'W7J, A. G. -- lllle~i:juvtr.~itnt in a Dem-,nstration Cand
P~~da-,,og -;ci, jci 11,!s InA of Acad of P-!,I, j
I .; 1, ~Citncts
RjF-31'L, ~'V_;cco.,T l)53. (litf-rativrVy 7hurnal.-Fizilcr-1, Jail 4)
30: JWI: 168, 22 July 1954

PMOVSXIY, Aloksandr Androyevich; GIAZYRIS# Alskeandr Iyanovich; DqM
Aloks ZVORYKIN, Boris Sergeyev ich; SffURXHlH.
*ioiI'f.a:+O"O,' "VICH, T.Y.. redaktor; TSYPPO, R.T., takhni-
chookiy redaktor
[Demonstrative experiments in physics for classes 6 and 7 of the
secondary schools; teacherls manual) Demonstratsionnyo opyty po
fiziko v VI-VII klassakh orednei shkoly; posoble dlia uchitelia.
Pod red. A.A.Fokrovskogo. lzd. 2-oo. Moskva, Goo. uchobno-podagog.
izd-vo Kinisteretva proeveshcheniia RSISR, 1956. 270 P. (HLRA 9:12)
(PIqoics-Uperiments)

POROVSKIT. Aleksandr Androyevich: GIA AMIN. Alskmandr Ivanovich; JDUBOT
Aleksandr q#_&qr!T 11 , TCIRYXIII. Boris Sergeyevich; SA-Mi-Y.
7"-TICH, T.T., redaktor; WHATURT, S.G.,
takhnichookly redaktor
[Practical work in pbrics for senior classes of secondary schools;
a sanual for teacherej Praktikum po fivike v starshikh klaguLkh
sredtnet shkoly; posobte dlia uchitelia. Pod red. A.A.Pokrovskogo.
Isde 3-s, ispr, Moskva,, Goes uchabno-padagog. izd-vo Hinisterstva
prosveskW.heniia RSM. 1956. 288 p. (KLRA 9:10)
(Physioe-Probless, exercises. ate.)

DMOV. A.G. (Kooky&)
,~~
Teaching methods for machine-shop practice. Fiz.y shkole 16 no.l:
40-45 J&-Fe 156. (NLRL 9:3)
(Machine-shop, practice) (Technical education)

BEIODMKAToL. N,L; GALININ, D.D.; GORTACMN, U.N.; GUZYRDI, AOIS, D=T,_L.G?;
YEVROPIN. Tu.P.; TMKWDVICH, A,S,; ZVOMJLIN, B.S.;*IVANOT, S.17,e-~V,
V.V.; LAVBDVMT, X.7s; KU3MIN, N.Y.: HIKHEMV, To.Ta.; NABOEDY, X.Te.
PIRTMMN. A.V.; POWT, P.I.;"POKWVSKIT, A.A.;' RXZHIMV, L.I.; SAIMMV,
D.I.; SOMOV, I.I.; SOMWVA, U.N.; IMPHIK, E.Ta.; TUSIEDVICH, V.P.
Sergal Nikelaevich Zharkov. [Obituary]-Tizv shkols 16 n0-3:94-95 Ply4e 156.
(Zharkov, Sergai NikoUavich, 1883-1956) (MA 9:7)

DUBOW, A.G.; PARMOT, K.Ya.
Ways of strengthening school equipment for technical education.
Politakh, obuoh, noolot6g-79 0 157. (KLM lOt9)
1. Nauchno-inelodovatel'skly Institut metodov obuoheniya Amdeali
PedAgogichookikh nauk RSM,
(Technical education)

chi RIM. YU-Te., redaktor; SOLDLOYA, F.Y*,,
)U ~nichs~skiy r~sdakit
teekhnicheakir rodakto
0
(Practical work In school workshops; manual for workshop teachers of
grades five to seven] Prakticheekle zamtlia v uchebuykh masterskikh;
getodicheakoe posoble, dlia prepodevatelel truda T-Vil klassov. I(Ogkv&,
izd-vo Akadopedagoi,nauk R37M, 1957. 204 P. 127 P. of diagrams.
(Kanual training) (KIRA 10:5)

POKROVSKIT. Alsksandr An4zeyewieh. Prininall uchastiyes -41-AZY119,
A.I., nanobA" metmAn1k; NMOT, AA.o nauchnyy setraft1k;
ZVORTKIN, B.S.# nauohnyy moTtkTiMuMMIN, S.A., n4uohnyy
*otrtt4nIkj KOZININg. A.?~,c SljvW konctruktor; NIX9AUVITICK,
Toy., red#: IfixPPOO soy*: W&ROT"t
ClIquipment of a physical Isborstoryl teacher's mumall
Oboradayanio fisichaskogo kalbinstal posobie dlis uchitelia.
Moskva. Gom.uchebuo--psdagog.Ixd-vo X-va prosy. R575R. 1958.
422 P. (NIn 12:7)
.1. Upraylenlys mobabno-tekbutchaskoji promyrhlennosti.
(Physical laboratorlos-Iquipmat and supplies)

JPCKROVSKIY, A.A., kand.podagogenauk, starshiy nauchnyy sotriidnik;
BUROV, V.A. uchitell ; OLAMIN, A.I., starehly nauchnyy notrudniki
pensioner; 60T, A.G., starshly nauchnyy sotrudnik; ZVOMEN. B.S..
0. - d
nauchnyy a tYu-d7Av!-rARff-ft%KrT, S.Te., uchitall; KOSTIN, G.N., pro-
podavatell; MIRGORO=IT, B.Tu., uchitall; OREKHOV, V.P., prepoda-
vatell; O11LOV, P.P.. propodavatell; RAZUMCVSKIT, V.G., aspirant:
MIKTANTM. I.M., aspirant; TMUMTITXT, M.K.. prepodavatell-,
KHOLTAPIN, V.G., prepodavatell; SHAKHKAYNV, N.M., nauchnyy sotrudnik,
uchitall-, VOYMIKO, I.A., uchitell aredney shkoly, pensioner; STA-
HOSTIN, I.I., prepodavatell; KOGILKO, A.D., aspirant; SHMIN, N.K.1
KOPINKOVA, L.A., red.; LAUT, Y.G., tekhn.red.
[Now school equipment for use in physics and astronomy) NoVye
shkolinye pribory po fizike i astronomii. Pod red. A.A.Pokravokogo.
Moskva, Izd-vo Aknd.pedagog.nauk RSM, 1959. 161 p. (MIRA 12:11)
1. Akademiya pedagogicheakikh nauk RSFSR, Moscow. Institut metodov
obuchanlya. 2. Laboratorlys matodiki fiziki Inatituta wtodov obuchs-
niyu Akademil pedagogicheskikh nauk RSM (for Po)=ovBkiy). 3. Sred-
nyaya zhelesnodorozhnays shkola st.Kratovo, Moskovskoy oblneti (for
-Burov). 4. Institut metodov obucheniya Akademii pedagogicheskikh uauk
(for Glasyrin, Dubov, Razumovakiy, Rumysntsev).
(ConGinued on next card)

PMOVSKIY, A.A.-(continued)'Card 2.
5. Institut metodov obuchenlya Akademil pedagog.nauk; srednyays shkola
No.315 Hoskvy (for Zvorykin). 6. Srednvays shkola No.212 Moskvy (for
Xamenetskiy). 7. Krasnodarekly pedinstitut (for Kostin). 8. Srednyayn
shkola Ho.18 g.Bumy (for Mirgorodakiy)i 9. Avazanskiy pedinstitut (for
Orekhov). 10. Stalingtbdakiy pedinstitut (for-Orlov)..Il. Hookovskiy
dorodukoy pedinstitut; arednyaya shkoln No.443 Moskvy (for Terentlys-T).
12. Balaahavakiy pedinatitut (for 101olyapin). 13. Institut metodov obu-
cheniya Akademii pederog.nauk; srednyaya shkols Ho.215 Moskvy (for
Minkhwyev)e A, Moskovskly pedinstitut im. V.I.Lenina (for Starostin).
15. Podinatitut im. V.I.Lenina v Mockve (for Mogilko). 16. Zaveduyu-
shchiy narodnoy astronomichaskoy observotori~ey Dvorten kulltury Hookov-
skogo nvtosavoda im. Likhnchava (for Semakin
. (Physical instruments)

MBOV, A.G. - ~
Training for work in the eight-year schools. Politokh.obucb. no.2:15-19
F '5 9. (HIRA 12:3)
(Manual training)

POKROVSKIY, Aleksandr Andeyevichj BUROV, Vladimir Alekseyevich;
.GIAZYRIN, Aleksandr Ivanovich; DUDOV, Aleksandr
Grigorlyevich; ZVORYKIN, Boris Sergeyevich; RIWANTSEV,
1van Mikhaylovichl MLOV, L.S., red.; KREYSp I.G.p
tekhn. red.
(Laborator7 maw eco
ial on dies in a ndary schools; a
pp
teacher's manuaij PraktiLli po fizike v srednei shkolej
posobie dlia uchitallao (By] A.A.Pokrovskii i dr. Izd.4.
perer. Moakvav UchpedgIz$ 1963. 223 p. (MIRA 17:3)

TKACIIEVp */.V... inzh.; inzh.; OGANESOV, V.b'., Irz;,.; ANT!"EM,
IM., inzh.; WAX, R.R.P inzh.; NOCTCZET-S,
1..:'fectiveness of grinding in mills of closed and opan cycles.
!',Iement 31 no.2sl3-14 Mr-Ap 165. (Mffli 18:8)
',, Gosudarstvennyy vsesoyuznyy institut po proyektirovaniYu i
r.4 uchno-isoledovatel I skim rabotam tsementnoy prumy3h1ennosti,
L!ningrad, i tsomentnyy zavod IIPunLne Kunda".

A
)tan. I Lnstr. 24/4, 17 19, April
T. . .....
MU

25M P. _~ PHASE I BOOK EXPLOITATION SOV/1257
Moscow. Stankoinstrumentallnyy institit. Kafedra "Instrimentallnoye
proizvodstvo."
Novoye v konstruirovanii metallorezhushchikh In8trumentov (Recent
Developments in the Design of Metal-cutting Tools) Moscow, Mash-
giz, 1958.' 229 P. 5,000 copies printed.
Ed.: 3emenchenko, I.I., Professor; Ed. of Publishing House; Balandin,
A.F.; Tech. Ed.: Gerasimova, Ye.S. and Uvarova, A.F.; Managing Ed.
for Literature on Metal Working and Tool Making (Mashgiz): Beyzell-
man, R.D., Engineer.
PURPOSE: The book is intended for engineers and technicians of the
machine-building industry.
COVERAGE: In this collection of articles results are presented of
investigations carried out at the chair of "Tool Making" of the
Moscow Machine Tool and Tool Making Institute imeni I.V. Stalin.
The articles discuss new features in designing highly productive
metal-cutting tools.' : generating cutters, cutter gear generating
heads, hobB and gear shaper cutters for cutting gears for subse-
Card 1/3

Recent Developments (cont.)
SOV/1257
quent shaving, of flat broaches for broaching bodies of rotation,
and circular broach cutters for cutting straight level gears with
circular tooth profile. Problems of definition and the clasalfi-
cation~'of metal-cutting tools are also investigated. The role of
Russian toolmakers claimed to be the first in the world to manu-
facture rifles with interchangeable parts is related. No persona-
lities are mentioned. There are 24 references, all Soviet.
TABLE OF CONTENTS:
Foreword . 3
Sakharov, G.N., Stalin Prize Winner, Candidate of Technical
Sciences, Docent. Design of Round Generating Cutters 7
Mayushin, V.M., Candidate of Technical Sciences, Docent. Some
Problems in the Design of Cutter Gear Generating Heads 59
Voroblyev, V.M., Stalin Prize Winner, Candidate of Technical
Sciences, Docent. Geometric Parameters of the Cutting Part
of.$ingle-point Tools With Large Cutting-edge Angles 96
Card 2/3

Recent Developments (Cont.)
SOV/1257
Dubov, A.N.. Candidate of Technical Sciences, Docent. Tools
r6r Cutting Gears for Subsequent Shaving 107
Voroblyev, V.M., Stalin Prize Winnero Candidate of Technical
Sciences, Docent; and Engineer Ye.C. Dolaik. Profiling
Disc-type Milling Cutters for Cutting Helical Grooves With
.Large Helix Angle on Hobo 130
Furman, L.L.., and A.M. Leyn. Problems in the Theory of
Broaching Rotation Bodies With Flat Broaches 141
Ganopolskiy, L.Z., Engineer. Some Problems in the Theory
of Circular Tooth Profile Gearing and Designing Tools to
Cut Them 167
Frezerov, G.R. Professor. The First Russian Toolmakers
(Historicall - 202
Matyushin, V.M., Candidate of Technical Scienceso Docent.
Definition and Classification of Metal Cutting Tools 213
AVAILABLE: Library of Congress G018fm
Card 3/3 3-26-59

DIJBROV, A.P.
Simple method of ultraviolet microirradiation with the use
of a reflectIng optic system* Radiobiologiia 3 no*2017-320
1 163 ' (MIRA 17:1)
'I. Institut biologicheskoy fiziki AN SSSR, Moskva.

_UUDUV)_A*_QA____
S-5-14o 551-551-551-506.5
Garidin,, L. S. and Vubovy A* S., [The complex expedition of 194T
for the study of atmospheric turbulence. Leningrad. Glavnaia
Geofizicheskaia Observatoriiap Trudy, 16 (78):5-9t i94777=P .
append. p. 136-143. --A series of observationso devoted to all
aspects of atmospheric turbulence., was made at the station Dolgoprudnaia
(near Moscow) in order to test theoretical formulas proposed by
BUD=, IAINIMAJI, ERM and others. 'Llds paper serves as an intro-
duction to 11 papers., published in the aw~e volume,, and describes
the general conditions of the expedition, the program of measurements
and the location of instruments. The appendix presents profile
data for temperature (surface,, 0.21 0-55~ 20 m), and data for the
radiation balance and weather conditions. The time distance is 20
min (for 15 days~ but the conditions during the might are not
covered.

5.5-136 551-551-551-508,53
Dubov, As S., nDetermination of the velocity of wind gusts in
airplane soundinV by means of accelerometer records." Leningrad.
(31svnaia, Geofizicheakaia Observatoriia Trudy, 16(78):85-92, 1949-
5 figs., tables, 0 refs.., 7 eqs. MC--The Vertical velocity of vind
gusts and the coefficient of exchange in the free atmosphere can be
computed by means of accelerometer records) made on an airplane,
considering the air density.. the weight and wing spread of the plane,
etc. The author analyzed a set of eight differential equations, but
failed to solve them, and proposes ajim~lified solution, which
considers only larger eddies (over 7 8 m). An analysis of possible
error is made. Samples of computations am presented, showing the
superiority of the author's equation, which considers also the
veitical velocity of the plane itself. A nomogram facilitates
practical computations.

VORONTSOV, P.A.; DUB21&.1-5-
Methods of investigating the structure of air currents from and
airplane. Trudy 000 no.51t50-65 '55. (MM 9:8)
(Atmosphere) (Aeronautics In meteorology)

GANDIN, L.S.; IMBOT, A.S.
Qualitatt" ana4vis of the vortex equation. MetecrA gidrol.
no.4:36-37 Ap 157. (Atmosphere) (KLRA 10:5)

/ J -~Y / "f -, ,I- - '-I- -')
;-, ~ ~ ~,~ -11 . I I ,
GANDIN. L.8.; DUBOT, A.8,j SOLOTITIT, T.A,
-- mmwmwwmm
In the Toeikov Main Geophysical Observatory. Meteor. I gidrol.
no-8:70-72 Ag 157. (Meteorology) (KLBA 100)

36-7X-2/16
AUTHOR: Dubov, A. S., Orlova, L. S.
TITLE: Results of Forecasting a Surface Field of Pressure and
.Mapping of Beric Topography by the Graphic-analytical
:Method (Rezulltaty prognpza nazemnogo polya davleniya 1.
kart baricheakoy topografli grafo-analiticheakim.
metodom)
PERIODICAL: Trudy Glnvncv Reofizicheskoy observatorii
1957, Nr 71, pp. 34-48 (USSR)
ABSTRACT: The forecasting method described by M.I. Yudin (this
publication, Pp- 3-331) is described and evaluated. The partic-
ulare of selected units and practical steps in the formulation
of the method were given, and the argas for Which the material
was collected are cited. A major point is made of the calcu-
lated transfer of pressures and three separately ledding air
streams. The efficiency factor for successful progn6stication
may range from 96 percent In summer to 24 percent in autumn.
All predictions are based on the correlation of calculated and
actual values which, in general, are difficult to establish.
New indices of possibly lesser precision are recommended for
Card 1/2

36-71-2/A
Results of Forecasting a Surface Field of Pressure (Cont.)
this evaluation. On the whole, the predictions for surface
baric fields are more reliable than those for the 500 mb. our-
face. Of thespecial c6mponents, the advection of temperature
is better reflected in the findings than the advection of the
vortex. At the same t1ite, synoptic forecasting methods are
better justified-pereentage-wise) than analytical mezhLde Which
provide no advantage In kicking up the emerging baric compo-.
nents. The insufficient -weight" given to advectian by tempera-
ture is a major source o..' error,, however, the basic weakness
of analytical schemes is.seen in the unsatisfactory follow-up
of the Intensification of bario formations. Correlations of
probability are given for all types of baric situations, such
as, cyclonic, anticyclonic and mixed. The failure to forecast
developmert of the Leningrad cyclone which caused an inundation
in Sept. 1955 is attributed to a failure of graphic integration
and to some errors In evaluating various surface factors. Use
of electronic com uters is strongly recommended. Persons men-
tioned include: ~udin, M. I... Dubov A.S..,, Orlova, L.S. There
are 7 figures, 11 tables, ahd 3!n-r~;Ki_e~_c;; of which 2 are USSR.
AVAIAABLE: Library of Congress
Card 2/2

Aj~
iUTHOR: Dubov, A. S.
TITLE: -imiumon 'of surface
Field of Pressure on
~reniya prijprognoze
+Mdy
36-71-4/16
Friction in Forecasting the
the Ground (Ob uchete prisemnogo
polya dayleniya u zemli)
Olavnoy geofizicheakoy observatoril
PHRIODICALt
1957, Nr 71, pp. 66-71 (USSR)
ABSTRACT: The Central Institute of Forecasting has thoroughly
analyzed the effect of turbulent friction on the variation of
pressure. This is used by H. I. Yudin in his study of the flow
of an ideal liquid'i.e., that vertical velocity of the ground
friction at the surface is not zero but is proportional to the
Laplacian of surface pressure. Proof is,given that equations
for vertical turbulent transfer alter the relationship between
temperature and spatial derivatives of the geopotential. At a
later stage is appears that this factor of transfer to some-
what overvalued. The mathematical characteristics of the ini-
tial field are expressed by first derivatives of pressure1n
time restricted by some limiting conditions The graphic-
analytical method is applied to evaluation ;f the pressure
factor and to*the schemes used in the solution of the problem.
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36-71-4/16
ivaluation or-Pressure on-~he 6r6und (cant.)
An Illustration of the-actual findings is giverr and the effi-
cienc'y of this method-of forecasting is evaluated. Therie are I
figure, 3 tables.and 2 USSIf references.,
AVAILABLE: Library of Congress
Card 2/2

DUBOVJI
DLBOV A S. and STOLYAROVA G. V.JO 'Experienco in Forecasting Temperature
Using by6~odynamic Methods, P- 30
3TOV A. S.., "Influence of Pountein RanCes on the Dinplacement of Cyclones." p. 40
j_
PUblIcation: Voprosy dinovdcheskoy meteorolo,,111 t thorit klivatA (Proble.T,.s In
Dyns3mlc Mpteoroloay and the 7heory of Cliwte.) IAnin_arad , GIdroTreteoizdat,
1953. 125 p. T17djv Glayneye geofizicheakeja observatorlyn Lenlnr,~Tad, VYP. 76,
The collection of 9 articles deals with problems in dynemic wteorology,, 'the
theory of climate, end the foreceatirg of rir temperature uslAe elemnts
of tho therobBydrodynamic theory, A uystein of clImetological rsSionalization
for the USSR is analyzed end recent pertIment date in thib retZard shown Srpphicnlly.

44
gq
ifib
41
IK
1 43
L " i '

A. S.
AUTHOR: ~Lbov
S/531/59/000/098/001/005
TITLE: Lateral Aircraft Oscillations Caused by-Wind Gusts
SERM: Leningrad. Mavnaya wofiticheakaya observatoriya im. A. I. Voyeykova.
Voprosy avialisionnoy meteorologii, 3-16.
Trudy, no. 98, 1959
TEM. A formula is derived in order to associate lateral aircraft oscillations with
horizontal wind gusts. The establishment of this association is necessary because
present accelerographs do not reliably determine the magnitudes of horizontal gustsp
which, upon analysis, play a much greater role than the vertical in creating lateral
aircraft oscillations. From well-known equations describing lateral motions of air-
craft, the author generalizes expressions describing individual increments of aero-
dynamic forces and moments in the aircraft's boundary layerl resulting from changes in
flight attitude angles as turbulent motions are encountered in the onflowing airstream.
The author notes that as a result of the V-shape of the winds, vertical gusts may cause
lateral aircraft oscillations only if the vertical gust values amount to approximately
20 per cent of the horizontal gust values on the wings. This circumstance is most prob-
able at times when the variability of vertical velocities is abrupt . In establishin
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211U
S/531/59/000/098/001/005
Lateral Aircraft Oscillations Caused by Wind Quate
a relationship between horizontal gusts and lateral aircraft oscillations, the set of
equations derived is made for the simpler problem of uniformity of wind gustiness over
the entire boundary layer of the aircrafts that isp the wind has been averaged as a
single value. This set of equations can be used in solving the more comp2ex problem of
variability of wind gustiness if the gust fields aregiven. The solution of this set of
equations is made similarly to that for differential equations derived by M.I. Yudlhin].946
for describing longitudinal aircraft oscillations. By means of this solution it is
possible to obtain the statistical characteristics of the aircraft's oscillations, if
the characteristics of the wind gusts on the flight path are known. As an example,
the question of ratios between amplitudes of horizontal wind gusts and lateral acceler-
ations at the aircraft's center of gravity for turbulent motions of different frequen-
cies are analyzed. From this analysis'a, transfer function is obtained similar to that
for transfer functions for longitudinal aircraft oscillations. Concrete calculations
were made for Northrop-2-E aircraft, the aerodynamic characteristics of which were pub-
lished in in A.L. Raikh's work (Ref. 21 Trudyp TsAGI no. 458,1939) Conclusions: The
transfer function which is graphed shows that low-frequency lateral wind gusts are only
slightly reflected in lateral accelerations of the aircraft. As in the case of
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213.11
S/531/59/000/098/001/005
Lateral Aircraft Oscillations Caused by Wind Gusto
longitudinal oscillAtions, the derived formula is expressed in dimensional values and
is valid only for high-frequenoy turbulent motions. In order to determine the low--
frequency turbulent motions, the relationship between the transfer function and the
frequency7P be taken into account. It also was mathematically determined that the
sensitivity, accelerographs must be raised by one order so that the hor12ontal wind
Y a
gusts can be determined as accurately as the vertical gusts are presently determined.
The Russian abstract of this article appears In Referativnyy Zhurnal, Geofizika, 1960,
No. 11, Ref. no 14469. There are 3 references, all Soviet.
Card 313

AUTHOR: Dubov, A. S.
21114
S15311591MM81'e,f) , ln,~A
TITLEt The Relationship _%tween 14rbulence Barameters of Aircraft
Posselssing Different Structural Designs Under Identical
Meteorological.Conditions
SERIAL: 'Leningrad. Glavnaya goofizichaskaya observatoriya im. A. 1. Voyeykova.
Trudy, no. 98, 1959# Voprosy aviatsionnoy moteorologii,43-53.
TF,XTs A formula is derived whereby the characteristics of turbulence of one aircraft
can be determined if the turbulence characteristics-of another aircraft under identi-
cal meteorological conditions are known. The derivation of this formula was under-
taken in order to establish a relationship between the degrees of aircraft turbulence
for two aircraft possessing different structural designs but flying In the same air
mass or under identical meteorological conditions. It is well known that two air-
craft with different stability characteristics will react differently to turbulent
air motions encountered in the main onflowing airstream on a flight made under iden-
tical meteorological conditions or in the same air mass. Of the presently available
Card 113

21M
S/531/59/000/098/004/005
The Relationship Between Turbulence Parameters of Aircraft...
recording instruments for registering the effects of the atmospherets turbulent
motions, the accelerograph most readily and reliably records the vertical components
of the acceleration at the aircraft's center of gravity. Although aircraft turbu-
lence involves manifestations other than phenomena associated with vertical over-
loads (yawing, banking, abrupt lateral thrusts, etc) nevertheless for a general
evaluation of aircraft turbulence vertical overloads are adequate. A. S. Dubov
(Ref. 5: Trudy GGO., no. 81; 19591 made an analysis of the attendant errors and cer-
tain recommendations pertaining to a number of approximate methods now being used to
associate recorded vertical aircraft overloads with vertical components of wind gusts
In this article is used an approximate method obtained in one of A.S. Dubov's earlier
works (Ref. 6: Trudy, GGO.p no. 16(1949); this method*gives good results for stable
aircraft, and can be used to derive the formula. According to this approximation,
the following equality must be realized where uz(t) is the vertical component of the
wind gust, n(t) is the vertical acceleration at the aircraft's center of gravityp b
is a coefficient depending on the aerodynamic characteristics of the aircraft and on
the flight attitude. C is a constant of integration determined from the condition of
equating the uZ value, which has averaged over a fairly long interval of time, to zero.
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21114
S/53l/59/000/098/CQ'W"V^,35
The Relationship Between Turbulence Parameters of Aircraft...
There ist howeverone difficulty. It is impossible to equate values of the vertical
wind speeds in the passage by the two aircraft of the same point in spacep since
the two aircraft, pass this point at different moments of time in a field of vertical.
wind speeds where there also is temporal variability. Hence, after making the re-
quired formulated evaluation of the variability of vertical wind speeds with respect
to both time and spacep the formula being sought is readily derived; From this evalu-
ation it was determined that if the aircraft speed is considerably greater than that
of the wind, then it may be assumed that the aircraft penetrates a stationary field of
wind gusts, but naturally only for brief intervals of time. In -asing the derived for-
mula for practical purposes, actual numerical calculations were made for determining
overload values for a LI-P aircraft from known overload values of a PO-2 (biplane)
aircraft. The calculations were then compared with experimental data obtained by
paired flights of these aircraft (eight cases). In comparing the calculated results
of two other approximate formulas widely used with those of the author's derived for-
mula it is seen from the graphed results that the author's formula is the most accu-
rate. The Russian abstract of this article appeared in Referativnyy Zhurnal,
Geofizika, 1960, No. 11, Ref. No. 14470, p. 168. Thera are 6 references, all Soviet.
Card 313

j"SWO (;Z,2 oj~ /of -3 21115
3,.51410 (,,~-30S~ ~YOS-) S/531/59/000/09/005/005
AUTHOR: Dubov, A. S.
TIT Determination of the Turbulent.Exchange Coefficient From an
Aircraft's Acceleration
SERIAL: Leningrad, Glavnaya 1~,eofizicheskaya cobservatoriya im. A. 1. Voyeykova.
Trudy, no. 98, 1959, Voprosy aviat6ionnoy meteorologii,.54-67.
TMCT: A fornula, is derived and verified for calculating the turbulent exchange
coefficient in the free atmosphere, that is, at levels above the surface layer of
the atmosphere. There were two reasons why this problem was undertaken:
1) existing methods for calculating this coefficient at levels above the surface
layer of the atmosphere, especially in the 100-2000-meter layer, had not been
substantiated by other independent methods and were, therefore, considered less
reliable than the still imperfect but well substantiate& methods used for calculating
the exchange coefficient in the surface layer of the atmosphere, 2) vertical
gradients of the various meteorological elements upon which calculations have been
based and so reliably mad for the surface layer, are less pronounced in the free
atmosphere. Of three well known structural methods used for calculating the
coefficient in the planetary boundary layer, only E. S. Lyapin's method
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21115
Determination of the Turbulent Exchange Coefficient ... 8/531/59/000/09/005/00i
(Ref. 9: Meteorologiya i gidrologiya, 1948, no-5) can be generalized for deriving
equations making it possible to use acceleration and air speed data recorded by
aircraft for calculating the exchange coefficient. In 1950, the author generalized
Lyapin's formula for expressing the coefficient of turbulent exchange in terms of
acceleration and speed characteristics recorded by sensimg elements of instniments
installed on aircraft in flight as follows:
k D V
Z
2
where k is the coefficient of the vertical turbulent exchange, uz is the mean
(taken7absolutely) value of the vertical wind speed., D is the mean duration of a
vertical velocity of the same sign, V is the mean (taKen absolutely) velocity of
the recorder, sensing element with respect to the air, ux is the mean (taben
absolutely) value of the horizontal wind gusts. if the recorder's sensing element
is stationary with respect to the earth., then equation (1) reverts to Lyapin's
formula. In this case the recorder's sensing el*ment measures the mean wind speed
(that is, if the pulsations are considerably less than the mean speed) so that
equation (1) is rewritten as U2
k 0 z D U
2 u. (2)
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21115
Determination of the Turbulent Exchange Coefficient S1531159100010910051005
where U is the mean wind speed. If the recorder's sensing element moves si-11-
taneously en masse with the air mass engulfing it, then V w N and equation M
t~ Ow #Am ao HosoolborgId atmturkl wthod fomlrA (Kof. J: Atim. 4or kd1wr.
Bd. 57, 191-17). The third or Ertel's structural wtbod could not be used because
L. r. ah,~herb4wya (Rot. loz Trudy 000 no. 16 1781 1949) and 1. S. Borushko
(Ref. 10: Trudy GOO no. 16 [781 1949) had shown in their critical analysis that
certain hypotheses upon which his method Is bawd can not be substantiated. At
present, accelerographs do not reliably determine gust values. But nryertbeUar,
in the free atmosphere, velocity pulsations with a considerable degree of accuracy
may be assumed to be isotropic, that is % a u x or an assumption upon which
equation (1) acquires the form k -us Uj
2 (3)
The value of u., as vas discussed above., was found by means of the relationship
uz 0 bn
(4)
where n is the acceleration of the aircraftts center of gravity expressed in
percentages of the acceleration of gravity, b Is a coefficient of proportionall
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21115
Determination of the Turbulent Exchange Coefficient ... S/531/59/000/09/005/005
depending on the aerodynamic characteristics of the aircraft and of the flight
attitude. This coefficient was determined from another of the author's work in
the present symposium (Ref. 17: Trudy 0GO no. 0,, 1959).
Results and Conclusions. Completed calculations indicate that formula (3) gives
entirely reasonable magnitudes of the coefficient, IS. In particular., this is
made apparent by comparing magnitudee of the coefficient obtained from gradient
observations' data in the surface layer extrapolated up to flight altitude on the
assumption that k Increases linearly with altitude up to a level of 30 to 50 meters
above which it r9mains constant. Certain data on the diurnal variations and of the
k coefficient profile aloft determIned from aircraft observations mad jointly by
the Central Geophysical Observatory and the Central Aerological Observatory at
Moscow and by the Central Aerological Observatory In the vicinity of Tbilisi in the
81 r of 1947.. were obtained. In comparing his results with 'earlier Investigators
concerned with the problem of calculating the exchange coefficient in the 100-2000-
meter layer, the author believes their calculated values are too low,, in particular
those of Laykhtman anA Chudnovskiy (19491 and Kildner 11939). M. P. Cbulnovu
(Ref. 5: Trudy GOO no. 28., 1951),, P.A. Vorontsoy (Ref 15: Trudy GOO no. 39.. 1953)
and others have come to the saw conclusion. Two explanations are given for this
circumstance: 1) an aircraft is unable to react to turbulent formations of very
small scales owing to its inertia and in the case of very large scale turbulent
motions, the aircraft is seized by air mass engulfing it and ascends and descends
en masse with it. 2) the final formula (4) is valid only for pulsations of high
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213-15
Determination of the Tarbulent Exchange Coefficient ... S/531/59/000/09/005/005
frequencies., that is., pulsations of small scales. In addition,, a third possible
reason is the assumption of an approximate uniscalar nature of turbulence found
in implicit form in the derivation of Lyapin's forwala. The exticle presents a
fairly detailed survey on the status of met33ods anct results of determizing the
turbulent exchange coefficient in the atmosphere. The Russian abstract of this
article appears in Ref. Zhar. Geofizika 1960, no. 12, as Ref. no. 15968. There/
are 20 references,9 all Soviet,
Card 5/5

logs
I 3t
is
91
PIT
3 JAA 2j3 1 A Oo
its a

GAUDIN, L.3- Etranslator], red@; VMT, A.So Etranslator). red.; TLASOTA,
Tu.V., red.; VLADIKIROV, O.G.Tt-elifiE-ivd.
[Numerical methods of weather prediction; collection of translated
articles] Chislennys matody prognoss pozody; abornik parevodnykh
statei. Pod red. L.S.Gandina L A.S.Dabova. lenin&Tad. Gidro-
mateor.isd.-vo, 1960. 281 p. -'-- (KIRA 1):12)
(Weather forecasting)

DUBOT, A.S.
Orographio influquee on the motion of baric centers, Reteor.1 gidrol.
no.7:3-8 Jl 160. (KIU 13-7)
(Winds) (Mountains)

bh593
S/16 62/000/012/054/095
D228YL)307
z,,.UTHOR: 1~ubov. A.~;.
TITLE,: Forecasting the gnopotential field in the lower
k3
stratosphere
i'i~1-,1I(JDICj1L: .1cferativnyy zhurnal, Geofiziha, no. 12, 1962, 52,
abstract 123339 (In collection: 'Eaterialy Sovesh-
chaniya Koordinats. komis. po chisl. netodam prog-
noza, L., Gidrometcoizdat, 1961, 55-62)
Ti:XT: Cm the grounds of analysis of statistical material
(correlative relations bet--cen local tonjerature ch~-ngfcs and verti-
cal vnlocitics on the one hand, and vertical velocities and tempera-
ture advections on the other) it is shoi-m that for conditions of the
lower stratosphere the local derivative of the temperature can be
disregarded in the heat inflow equation. The soundness of this Sim-
plification Jis confirmed by analysis of the general solution Eor
the problem of finding vertical velocities from-the gcopotential
field. The existence of an "average level" analog for the vertical
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S/169/62/000/012/054/095
ForecaotinIt, the, gLO,)otCIItiiII ... U223/D307
velocity is considered. The sim?lifications introduced allow a
two-dimensional prognostic equation to be constructed for the 200-mb
U
surface geopotential. Unlike the barotropic schcnic the right-hand tA
Side Of this equation contains the temperature advection. Integx:a-
tion, with respect to time is carried out graphico-analytically an
a 'qJral-l" machine. The justification characteristics in 8-day mat-
erial are given.
Z-A,bstracterls note: Complete translation7
Card 2/2

DUBOV A.S.j NOBYAKOVAS A.A.
. -
Problem of AT3oo forecasting. Trudy GGO no.121:5%-66 161.
(KIRA 15:5)
(Weather forecasting)

DUBOV, A.S.
Determination of vertical gusts of wind from vibrations of the
airplane in flight, taking the pilot's action on the controls
into account, Trudy C40 nool2ld0gh-124 161* (mm 1515)
(Aaronautioa in mateor6jW) (Winds)

VJBOV I A.S.
-
AL11-Union Scientific Meteorological Conference divoted to
the 40th anniveroary of the Hydrometeorological Service of
the Soviet Union. Izv. AV SM. Ser. geofiz. no,1~138--]J+l Ja
162. WIRA 15.2)
(Meteorology-Congramees)
0'

S/331/62/0001135/0011002
1006/1206
AUTHOR:
TEXT: On determination of spectral density of vertical gusts from airplane oscillations
SOURCE: Leningrad. Glavnays gooflzicheskaya observatoriya. Trudy no. 135, 1962. Voprosy
fiziki pogranichnogo sloya atmosfery, 33-40
TEXT: A method for construction of spectral density of vertical gusts is dcicrib.-d using simultaneous
registration of angle of pitch and airplane overloading. The proposed meth,.)d provides the basis for
more reliable information about the spectral density of gusts in a larger frequency range (from the low frequ-
ency side). An example is brought of the calculation based on registrations of air?lane's disturbed motion in
an actual case. There are 3 figures.
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~
Effect of static stability on changes In preanure and the
forecasting equation for the lower atratosphere. Trudy GGO
no.12039-47 162. 17:6)

ACCESSION Nlt: AT40686s 8/2"1/63/000/143/0014/0022
AUTHOR: Dubov, A. S.; Kobyakova, A. A.
TITLE: Experience in forecasting the fields of pressure, temperature and
vertical currents in the lower stratosphere.
SOMCE: Leningrad. Glavnaya geafitichookaya observatoriya. Trudy-*, not 143#
1963, Voprosy* chislennogo prognoza i struktura meteorologichaskikh poley (Pro-
blems in numerical forecasting and structure of meteorological fields), 14-22
TOPIC T41GS: troposphere, meteorology, baroclinic quasi-geostrophic model,
weather forecasting, atmospheric pressure field, air temperature, air pressure,
atraospheric vertical currents, stratosphere, lover stratosphere, atmospheric
geopotential
ABSTIUCT: The results of 13 one-day and two-day forecasts of the geopo~tential
and temperature fields for the 200 millibar level are analyzed. The choice of
the 200-mb level in not ideal but was selected because data wore not available
for higher levels. A baroclinic quabi-goostrophic model is us6d. Temperature
forecasts for 48 hours in advance were successful, as illustrated by Enclosuri.
Correlation of the fields of vertical velocities, computed for the same period
dq,r,0e purpose of one-day and two-day forecasts, revealed no relationship

ACCESSION M: AT4016869 S/2531/63/000/143/0023/0026
AUTHOR; Dubov) A. S...
TITLE: Forecasting in the region of.tke stratospheric hi'gh-level frontal son*
SOURCE: Leningrad. Glavnaya geofixicheskaya observatoriya. Trudy*, no..143o
1963, Voprosy* chislennogo prognoza i struktura motoorologicheakikh poley (Pro-
blems in numerical forecasting and structure of meteorological fields), 23-26
TOPIC TAGS: meteorology, stratosphere, prognostic equation, weather forecast-
ing, atmospheric front, lower stratosphere, atmospheric geopotential field
JZSMACT: More precise two-dimensional progn03tic equations have been derived
for conditions in the lower stratosphere within the framework of the geostrophic
and adiabatic approximation. This is a further development of the author's pre-
vious work (Tr. GGO, No. 124, 1962). In that paper he derived a two-dimensional
equation for changes of geopotential with time, with expansion for a =all par-
ameter inversely proportional to the value of static stability. In derivation
of that simplified equation he neglected certain small terms, althougb allow-,
ance for them causes no difficulty. This paper cites refined prognostic equ&-
tion with the earlier discarded terms taken into account* In computing texua
Cord 1/2.-

ACCESSION NR: AT4016869
containing temperature it is assumed that isothermal conditions prevail, al-
though for the stratosphere this is true only as a mean, but since small terms
are involved there is no significant error. The author also presents now for-
mulas giving greater accuracy to determination of vertical velocities in the
initial equations of motion, which In practical prognostic methods ugually are
neglected, despite their importance. Orig. art. has: 11 formulas.
ASSOCIATION: Olavnaya goofisicheakaya observatoriya (Hain Geophysical Obser-
vatory)
sumiTTED: 00 DATE ACQ-. 2OP*b64 ENCL: '00
SUB CODE: AS NO R" SOV: 008 OMER. 001
Card 2A

BERLYAJM, M.Ye.;,DVBAV,-A.S. .
Mikhail Isaakovich lUdin; an his 50th birthday* Meteor# i
gidrol. no.12:55-56 D '63. (MIRA 17:3)

DUBOV, A.S.; ORIDVA, L.S.
Calculation of the movement of cyclones in mountalnous
regiona. Trudy GGO no.124:56-62 162. (MRA 17:6)

GEMJ11,11.A. ; DUBO.Vj A.S. (Leningrad)
"The aircraft as a meanB of atmospheric turbulence research".
report presented at the 2nd All-LTd6n Congress on Theoretical and Applied
I
1-:ochn.nics, I-Ioscow, 29 Jan- 5 Fab 64.

ACCESSION NR: AT4043147 S/2531/64/000/151/0041/0047
AUTHOR:j)ub_M_A.-S-(Cand1date of pbomico -mathematical sciences)
TITLE: Dotermination of horizontal wind gusts from accelerograph records
i SOURCE: Leningrad. Glavaaya geofizicheskaya observatorlya. Tr udy*. no. 161, 19".
Voprosy* chislennogo analiza I prognoza pogody* (Problems in numerical analysis and
forecasting), 41-47
TOPIC TAGS: wind, wind gust, meteorology, accelerograph, meteorological instrument,
aircraft overload, aircraft acceleration
ABSTRACT: The author clarifies the possibility'of determining horizontal wind gusts on
the basis of longitudinal accelerations of the center of gravity of an aircraft. The article
analyzes the contribution of the vertical and horizontal wind components in the formation of
longitudinal aircraft accelerations. It Is shown thatwith the exception of the sector of veryj
low frequencies the role of these contributions is Identical for a PO-2 aircraft. For
aircraft of the fighter type an approximate formula has been derived relating the
amplitudes of horizontal wind gusts and the longitudinal accelerations of an aircraft.
Several formulations of the problem are presented. It was found that the sensitivity of
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ACCESSION NR: AT4043147
I an aircraft to vertical gusts Is approximately eight times as high as to lateral hor-
Izontal gusts and twenty five times as high as to longitudinal horizontal gusts. no
accuracy of existing accelerographs ensures reliable measurement only of vertical
aircraft overloads. The reconstruction of the three-dimensional wind gust field from the
records of a three-oomponent accelerograph is Impossible due to the low sensitivity of
existing accclerographs. The solution of this problem requires instruments for recording,
accelerations of the center of gravity of an aircraft with a sensitivity one order of magnitude
greater than that of existing Instruments. Orig. art. has: 31 formulas, 3 figures and 2
tables.
ASSOCIATION: Glavnaya. pofizichealmya observatorlya, Leningrad (Main Geophysical
Observatory
suBmITTED: 00 ENCL: 00
SUB CODE: ES NO REP SOV: 009 OTHER: 000
2/2
Card
_7 T-J

-ACCESSION NR: AT4043162 6/2531/64/ObO/154/0090/0098
AUTHOR: Dubov, A. S.
TITLE: Allowance for heat fluxes In temperature forecasting
SOURCE- Leningrad. Glavnaya pofizioheskaya observatoriya. Trudy*, no. 1654. Voprosy*
Mild atmo6fery* (Problems in atmsopherio physics), 90-98
TOPIC TAGS: meteorology, atmospheric temperature, weather forecasting, atmospheric
physics, heat flux, radiation, atmospheric turbulence, cloud cover
ABSTRACT: In this study, prepared In 1953 but only now published* the author computed
the changes In the mean temperature of the lower 5-km layer of the atmosphere resulting
from radiation and turbulent heat fluxes. Local temperature changes In the heat flux
equation are represented as consisting of two parts; one part caused by horizontal heat
transport and the presence of vertical air movements and the second caused by the presence
of heat fluxes. As a simplification only heat fluxes associated with turbulence and radiation
processes are considered; condensation processes are neglected. The study is therefore
confined to computations of heat fluxes for anticyclonlo weather with few clouds. The
difference In radiative heat fluxes is computed directly by the Shekhter method. TUrbulent
Card 1/3

ACCESSION NR: AT4043162
heat fluxes are computed using the formula Q T ' -K T where k is the
coefficient of turbulent exchange, andy Is the adiabatic or equilibrium gradient which Is
not dependent on the coordinates. The temperature gradient is obtained from the
stratification curve (sounding data).: The coefficient of turbulent exchange is determined by
one of two described methods. Information on temperature gradients at the 1000- and 500-.
mb levels is taken from the same temperature profile data used for -,.omputing the radiative
heat flux. In the layer between the 600- and 1000-mb surfaces the radiativ(, heat flux is
compensated In a cloudless sky by a turbulent flux which Is greater than the radiative flux
by a factor of approximately 2. Transformation corrections are introduced by the M. Yo.
Berlyand method. Two extreme cases are considered for determining the influence of
cloud cover. In the first it'Is assumed that cloud cover is fixed in space and that air
masses in their movement enter and emerge from these cloud formation j . Thesecond
(more realistic) case allows for the fact that cloud cover is not fixed in space but moves
together with aIr masses. The problem of directly or Indirectly taking the latter reality
into account is considered in detail. Orig. art. has: 9 formulas, 1 figure and 1 table.
2/3

ACCESSION NR: AT4043162
ASSOCIATION: Glavnaya poflzichankaya observatoriya, LenjWad (Main Geop4pical
Observatory)
SUBMITTED: 00 ENCL: 00
001
'SUB CODE: ES NO REP BOV-. 004 OTHER.

VORONTSOVP P.A.; GERMAN, M.A.~ A.S.
Methodology and some results of an airborne exploration of turbulet
exohange in the boundary layer of the atmosphere. Trudy GGO no.158:
77-83 164. (MIRA 17:9)
Sk

L- 0-1515-66 FMT(1)/FGC - "M
iACCESSION NR: AT5017066 UR/2531/65000/16810014/0020
AUTHO? - D!Lbov A. G. , Turikov, V. G.
TITLE-. rorecasting the tropospheric pressure field
SOURCE- Leningrad. Glavnaya geofizicheskaya obsematoriya. Trudy, no. 168, 1965.
,Chislennyy analiz I prognoz pogody (Numerical analysis and weather forecasting),
~14-20
TOPIC TAGS: atmospheric pressure. weather forecasting. troposphere
,f,4 5
ABSTRACT: The three-dimensional equation for variattoni in presqitr,~ IS solved using!
the approximate boundary condition at tile lower edge of tht qtr4rospherq levived In
a pr-- P
-T-Iour, work. (Dubov, A. S., "On Forecasting in Stratosphnri- Vrr,w-al 7, e-
oirll~-!,., ~, 1, f
T)"1111Y ~;GO, No. 140, 1963):
+
flerf,~ io the altitude of the isobaric surface, 7 is temperatuve, g ic dceelendtlott
due to gravity, I Is the Coriolis coefficient, P Is the gas cotistdnt,
lCard 1/3
J

L 01515-66
ACCESSION NR: AT5017066
E2T Ya is the coefficient of static stability (y is the dr-I adiabatic terapera-
7
ture gradient), r. = P is the vertical coordinate in the isobaric system, r is,the
PO
quasihorizontal coordinate along the meridian from north to south, t is time. a and
are the symbols for Laplacian and Jacobian operators respectively. The deriva-
tion of this equation is based an a very simple and obvious fact, viz. an strato-
spheric isothermy. The approximate nature of the expression is due to the assump-
t;on that the cundition of isothemy is satisfied not only by average temperature
d"ctrit,ut~on, but, that Lndividual temperatures arelclose to isother-mal. Empirical
data have confirmed the applicability of this equation. The authors solve the well -
known problem of Buleyev and Marchuk (H. 1. Buleyev, G. 1. Karchuk, "on the Dynamlcsl
of Large Scale Atmospheric Processes," Trudy rFA AN SSSR, No. 2, 195e) an integratini
the equation
+ + dz R
X (21~
Vith variable U00de-bounda-r-7---c--o-n-d--I-tion- o olun
_tfo_ to- compared -with the Bultyev-
Marchuk results. it is found that there is very little difference between the two
C-4- 4- - - ____
7-7 7
Wes I~M~IWIF

ACCESSION NR: ATS017066
sets of results at ground level. Differences show up only at l&rge distances along
the horizontal. However, for practical purposes these diacreparcles have no effect
on --alciilation of The difference becomes more noticeable at higher levels.
Orig. art. has: 3 figures, 32 formulas,
ASSOCIATION: Glavnaya geofizztcheakaya- obset-vatoriyaj Lealugmd,
,Observatory)
SUBMITTED! 00 ENCL: 00 S
NO FIEF SOVI 005 OMR! 000
Card 3/,3
77%

ACCESSIOR ": AT5017067 UR/2531/65/000/168/0021/0026
A'JT1Q;?,: Dubov, A. S. ; I Lin B. K.
TIT U ~ Accounting for deviations of the wind from geostraphic in the boundary layer,
in nurmerical forecasting
SOURCV.: Leningrad. Glavnaya geofizicheakaya observatorlya. Trudy, no. 168. 1965.
chtslennyy apaliz i prognoz pogody (Numerical analysis and weather forecastli~q)
TO'- IC TAGS: geoatrophic wind, qeathgg for;,ecaqtLn-gt wind velocity
ABSTRACT: A modeL for the cop~ficient of turbulent intorch-ange is used in calcula-
"is ~D' 'h.,? winil in the houne-,3ry layer. According to -hisr nnAp! , the coefficient
'3 altilude an-1 71-le paT amp -
Lned tT--M data on the ge"t. 00,1C Vi-d arTd the E-3ULhneSS.
!of the underlying surface (Laykhtman, D. L.,, "'Physics of the Atmospheric Iloundary
Li-a-yer." GiLmrgt4oimrdat. Leningrad, 1961) using the equition for Mlan--o of t-.Irbu-
ind ~he r~elatlonsl,ip between wind vel---ity -P -,t,.fficient of Inter-
3 neight of one mer~r. Calculated values for the wir,d at tht vane level
!Card 1/2

--L-01516-66
fACCESSION NR: AT-5-011.7067
iere compared with weather map data. Ge-ostrophic vorticity and temperature advec
ti 1, o compared with the advections of these cam-- factors with regard to wind
'~)-,,undar-i --r A preiiminarv -z ~ha, the pro-
--ilat i -.T-.
fDI, ,
4,itions anfl high
1! I-S Orig. art tias 1 figure, I tabLe, 9 formj)as-
Glavnaya geofiticheskaya observatorlya, UP-ningn-id (Kain_ Geophysical
'r "
Observatory) q t4' I I
SUBMITTED: 00
ENCL: 00
SUB CODE: ES
NO PEF GOV: 008
OTHER: 000
~Card 212

VOLIFSON, I.S.; ARAMYAH, Ye.S.; DOBOV, A.V.
Obtalnlng stilfolone. NF3rtolwr. I naftokitim. no. 4:35- 47 01..
(mir-A 17:5)
1. Tatarokly neftyanoy nauchno-issledovatallskiy institut,
g. Rugmillma.

DUBOT, A.T.
Pbouliarities In the clinical aspects of tick-borne encephalitis
in districts of the rusnetsk Basin with differing couponents In
the population. Top.virue 2 no.61351-354 N-D 157. (KIRA 130)
i. ninum nerMkh boloney lovosibirskogo meditsitalrogo Insti-
tuta.
(KEMMVO PROVING11--X9010SALITIS)

DUBOV, A. Y.
Quinnerine snd seruntherepy in the Acute stage of tick-borie encepha-
litis; data from KemerovoProvince. [with summary in French]
Zhur.nevr i paikh. 58 no,W98-199 158, (MIRA 11:5)
1. Klinika nervnyU bolezney (sav.
meditainskogo instituts.
(ENCEPHALITIS, EPIDEMIC.
quinacrine & serother.
(WINACRINN, ther. use.
encephalitis, spidem.,
- Prof. D.T. luimov) Novosibirskogo
ther.
(Rua))
with scrother. (RURD

IWIMOT, D.T,; DUBOT, AeT.
Amyotrophic lateral sclerosis as a vernal encephalitis syndrome;
on the anniversary of the discovery and study of vernal encephalitis
by Soviet scientists. Zhur.nevr.i psikh. 58 no-3:282-287 158.
(MIRA 13:3)
1. Irafedra nervuykh bolesney (zaveduyushebiy - prof. D,T. Xhimov)
Novosibirskogo meditsinskogo Instituta,
(ANTOTROPHIC LATMM SCUROSIS, etiol Ophtbogen.
Russian t1ok-borne encephalitis ifts))
WGIPHALITIS. RP RIO. manifest.
amyotrophic lateral sclerO913 in Russian tick-borne
encephalitis (Ras))

DUBOVO.A.V.
Virologl~al diaposis of tick-borge anoophilitis by the tiague
oulture methcA. Vop. virug- 5 n6.414U,415 -To-Ag 160. (MIRA 101)
I
1, Kafedra mikrobiologii meditainskogo institutap Novosibirsk.
(ENCEPHALITIS) (TISSUE CULTURE)

1, DUBOV, A. V.
The use of tissue culture methods for the serological and virological
diagnosis of tick-borne encephalitis. Act& virol. (Praha) [Eng16 n&J:
58-65 Ja 062.
1. Chair of Microbiology, Novosibirsk Medical Institute, Novosibirsk,
and Department of Virologyt Institute of Experimental Medicine, U.S.S.R.
Academy of Medical Sciences, Leningrad.
(ENCEPHALITIS EPIDEMIC diag)

DUBOV, A.V.
Cytopathogenic action of thetick-borne ancephalitio virus on
hizmn and animal tissue culture collso Vop. virus 7 no.1:39-,43
Ja-F 162. (MM 15:3)
1. Kafedra mikrobiologii flovouibirskogo meditainakogo
instituta.
(EUCEPHALITIS)
(TISSUE CULTME)
(TICKS AS CARRIERS OF DIMME)

WDWO A.V.
Use of the tissue culture method for the difterentiation of
viruses of the tick-borne encephalitis group. Trudy Irk.
11.1 no. 7tl2l-126 162 (MIRA 19t1)
Interference between viruses of the tick-borne encephalitis
group and the R group. lbid.sI27-130
1. 1z Novosibirskogo meditsinakogo instituta.

,!fiftyl, ;,Ott. T.V. , j n7l'. K.V., inzh.;
ii,;,h..& BABICil, LOS.,, inzb.
tt.,
.thp-oving tho uonstructfW~ of high--,tLpw,.!f:f ~)rtn-hea7tl, Jurrianes
platit. rc-..F,:6(?4--697
Ag
IH 18:8)

DUBDVt, B,Ss-
Relation of Input and output valuen of multIcomponent devices.
Izm. tekh. no.Sil-4 Ag 165. (mm 18:9)

ACC NRo AP6025071
AUTHOR: Dubovp B. S.-
ORGs none
TITLE: Graphoanalytical method of processing measurement results
SOUCE: lzmeritelinaya tekhnika, no. 6, 1966, 15-18
TOPIC TAGS: measuring apparatus, data processing
ABSTRACT: A time-aaving graphoanalytical method is suggested for measurement-result
processing works its application to linear and nonlinear input-output relations
encountered in instrument calibrations is considered. (1) Linear relation. Parameters
n' and C of a straight line described by n w n' + CQ (where Q and n are input and
output quantities) are to be determined. 7he straight line is drawn through
experimental points, and deviations of experimental points from the line are plotted
in a larger scale in order to determine the mean square error. A numerical example
shows that the error In determining C by the above method does not exceed 0.1%.
(2) Nonlinear relation. Often the relation can be described by this polynomial:
n-n -'+CQ+C%Qs+c&Q,+...+chQ*. In this case, a monotonous curve is drawn through the
experimental points, and again (using tangent techniques) the curve of deviation of
points is plotted. Ordinarily, the equation of a second-order parabola is sufficient
Card 1/2 UDC:661.2.088019.281.2.001
CODE: UR/011516-6/000/006/0015/0018 f

ACC NR: AP6025071 0
for processing measurement results. Orig. art. has: 2 figures, 2D formulas, 1 table.
SUB CODEt 09, 13 / SUBM DATE: none

DUBOV, D.
Maintc-nance of machines and tractors durim- winter. p. 6.
U
Volt 6, no. 11, Nov. 1955
14al SF
I IINIZIEJONO MIEDELIE
Sofi,
ya., Dalgaria
So! Eastern European Accession Vol. 5 No. h April 19.56

SOLOVIYEVO S.P.0 kand.tokhn.nauk; inzhoj KOU40VSKOY, A.A.# lnzh.
Hermetic industrial buildings with exterior walls of glass reinfbreed
concrete* Prome stroio 41 no,,20-12 F 64a (MIRA 170)

DUBOV, I.Ye.
Turbulonce in quiescent prominenosse lxv,Xrym.astrofis.obser.
12:46-55) 154o (MIRA 130)
(Bun--Prominences)

DUBOT, X.Te.
Automatic guide of the coronagrapb at the Krym Astrophysical
Obsor7atory. Isv.Krys.astro,fis.obsor. 13:155-165 155.
OGRk 13.- 4)
(Electronic control) (Astronomical instruments)

DUBOV, B.Te.
IsotropIc turbulence and energy dissipation in quiescent
prominanceso Isy.Krym.astrofix.obser. 15:121-129 '55-
(MRA 13:4)
(Sun.-Prominswes)

DUBOV E.Ye.
.
Abundance of lithium In the sun. Astrou.tair. no.159,.11-13
MY,55- (KLHA 8:12)
(Lethium)(Spectrum, Solar)

- DUBOV, R. Yo.
Insturmental phntonffects.in photoelectric spectrophotometry
of the sun, lsv.Krym.astrofts.obser. 16:45-53 1%.
(HIRJL 13:4)
(Spnetrophotomatry) (Spoctrum. Solar)

:' rj';'%i.,~ "
DUBOV, E. Yet Cand Phys-Ilath Sol. -- (diss) *Speoial features of tho-Aneide WTSMW
and lwalneeeowe of protuberanoo8e" Len, 1957. 12 pp 22 am. (Acad Soi USSR.
Main Astronomical Observatory), 100 oopies. (KL, 15-57, 104)

SOV/124-58-11-12772
Translation frQjn: Referativnyy zhurnal, Mekhanika, 1958, Nr 11, p 121 (USSR)
AUTHOR: Dubov -E
TITLE: The Velocity Distribution in a Turbulent Medium and the Contours
of the Spectral Lines Emitted by the Nodes of Quiescent Prominences
(Raspredeleniye skorostey v turbulentnoy srede i kontury spektral'-
nykh liniy, izluchayemykh uzIami spokoynykh protuberantsev)
PERIODICAL: Izv. Krymsk. astrofiz. observ. , 1957, Vol 17, pp 199-210
ABSTRACT: It is assumed that a normal correlation 63tains between the
velocities of any pair of points in the turbulent medium. In such a
case the velocity-distribution function assumes the form
I (1-R) 1 /Z v2 - .
w(v) = Bf exp 2 ) dR, (1)
.0(1-R.20/2 201 (I-R2)
Here R = I - (ar2/3/2 c- ZI) is the correlation coefficient and a
is the standard deviation of the velocities. Formula (1) has the
Card I/Z shdpe of a Gaussian distribution but drops off more steeply. A

The Velocity Distribution in a Turbulent Medium(cont. )
SOV/IZ4-58-11-1277Z
comparison against this formula was performed for the velocity distribution of
clouds of interstellar mattir. The agreement was termed satisfactory. The
contours of the spectral lines were computed for the case in which the velocity
distribution obeys formula (1) with consideration of the thermal velocities of the
atoms. The contours differ only little from those computed for a normal dis-
tribution. The standard deviation of the turbulent velocities as determined
according to the normal distribution is 12-150/0 smaller than that actually
obtaining. In the absence of thermal mobility of the atoms this difference
incr'eases to 420/6. The selfabsorption effect is also taken into account.
Bibliography: 17 references.
S. A. Kaplan
Card Z/z

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