UNCLASSIFIED AD ARMED SERVICES TECHNICAL INFORMATION AGENCY ARLINGTON HALL STATION ARLINGTON 12, VIRGINIA UNCLASSIFIED

Similar documents
UNCLASSIFIED AD ARMED SERVICES TECHNICAL INFORMATION AGENCY ARLINGTON HALL STATION ARLINGTON 12, VIRGINIA UNCLASSIFIED

UNCLASSIFIED AD ARMED SERVICES TECHNICAL INFORMATION AGENCY ARLINGTON HALL STATION ARLINGT0 12, VIRGINIA UNCLASSIFIED

UNCLASSIFIED AD ARM ED SERVICES TECHNICAL INFORMATION AGENCY ARLINGTON HALL STATION ARLINGIN 12, VIRGINIA UNCLASSIFIED

UNCLASSIFIED Reptoduced. if ike ARMED SERVICES TECHNICAL INFORMATION AGENCY ARLINGTON HALL STATION ARLINGTON 12, VIRGINIA UNCLASSIFIED

Army Air Forces Specification 7 December 1945 EQUIPMENT: GENERAL SPECIFICATION FOR ENVIRONMENTAL TEST OF

UNCLASSIFIED 'K AD ARMED SERVICES TECHNICAL INFORMATION AGENCY ARLINGTON HALL STATION ARLINGTON 12, VIRGINIA UNCLASSIFIED

UNCLASSIFIED AD NUMBER LIMITATION CHANGES

UNCLASSIFIED. .n ARMED SERVICES TECHNICAL INFORMATION AGENCY ARLINGTON HALL STATION ARLINGTON 12, VIRGINIA UNCLASSIFIED

UNCLASSIFIED AD ARMED SERVICES TECHNICAL INFORMATION AGENCY ARLINGTON HALL STATION ARLINGTO 12, VIRGINIA UNCLASSIFIED

TO Approved for public release, distribution unlimited

THE INFRARED SPECTRA AND VIBRATIONAL ASSIGNMENTS FOR SOME ORGANO-METALLIC COMPOUNDS

UNCLASSIFIED AD Mhe ARMED SERVICES TECHNICAL INFORMATION AGENCY ARLINGTON HALL STATION ARLINGTON 12, VIRGINIA U NCLASSI1[FIED

UNCLASSIFIED AD DEFENSE DOCUMENTATION CENTER FOR SCIENTIFIC AND TECHNICAL INFORMATION CAMERON STATION. ALEXANDRIA. VIRGINIA UNCLASSIFIED

UNCLASSIFIED AD DEFENSE DOCUMENTATION CENTER FOR SCIENTIFIC AND TECHNICAL INFORMATION CAMERON STATION. ALEXANDRIA, VIRGINIA UNCLASSIFIED

TRANSLATION FOREIGN TECHNOLOGY DIVISION AIR FORCE SYSTEMS COMMAND [RD OHIO WRIGHT-PATTERSON AIR FORCE BASE

S 3 j ESD-TR W OS VL, t-i 1 TRADE-OFFS BETWEEN PARTS OF THE OBJECTIVE FUNCTION OF A LINEAR PROGRAM

UNCLASSIFIED AD Ail ARMED SERVICES TECHNICAL INFORMATION AGENCY ARLINGTON HALL STATION ARLINGTON 12, VIRGINIA UNCLASSIFIED

UNCLASSIFIED AD DEFENSE DOCUMENTATION CENTER FOR SCIENTIFIC AND TCHNICAL INFORMATION CAMERON STATION, ALEXANDRIA. VIRGINIA UNCLASSIFIED

UNCLASSIFIED AD NUMBER LIMITATION CHANGES

AO-A FOREIGN TECHNOLOGY.DIV WRIGHT-PATTERSON AFB 0ON F/G 13/7 MEMORY DEVICE U) MAR A2 N A PASHKIN, V N MALYUTIN UNCLASSIFIED FTD-ID(RS)T 0163

UNCLASSIFIED AD ARMED SERVICES TECHNICAL INFORMATION AGENCY ARLING)N HALL STATIN ARLINGTON 12, VIRGINIA UNCLASSIFIED

Reproduced DOCUMENT SERVICE CENTER ARMED SERVICES TECHNICAL INFORMATION AGENCY U. B. BUILDING, DAYTON, 2, OHIO

Conduction Theories in Gaseous Plasmas and Solids: Final Report, 1961

UNCLASSIFIED ADL DEFENSE DOCUMENTATION CENTER FOR SCIENTIFIC AND TECHNICAL INFORMATION CAMERON STATION ALEXANDRIA. VIRGINIA UNCLASSIFIED

TM April 1963 ELECTRONIC SYSTEMS DIVISION AIR FORCE SYSTEMS COMMAND UNITED STATES AIR FORCE. L. G. Hanscom Field, Bedford, Massachusetts

UNCLASSIFIED A ARMED SERVICES TECHNICAL INFORMATON A ARLINGTON HALL STATION ARLINGION 12, VIRGINIA UNCLASSIFIED

UNCLASSIFED AD DEFENSE DOCUMENTATION CENTER FOR SCIENTIFIC AND TECHNICAL INFORMATION CAMERON STATION ALEXANDRIA. VIRGINIA UNCLASSIFIED

UNCLASSIFIED A30 333~ ARMED SERVICES TECHNICAL INFORMION AGENCY ARLIGTON HALL STATION ARLINGTON 12, VIRGINIA "UNC LASS IFIED

UJNCLASSI FIED A D:FENSE DOCUMENTATION CENTER FOR SCIENTIFIC AND TECHNICAL INFORMATION CAMERON STATION, AI.EXANDRIA. VIRGINIA UNCLASSIFIED

"UNCLASSIFIED AD DEFENSE DOCUMENTATION CENTER FOR SCIENTIFIC AND TECHNICAL INFORMATION CAMERON STATION, ALEXANDRIA. VIRGINIA UNCLASSIFIED.

" EEEEEomhhEEEE EEEEEET. FI 9/5 PRINCIPLE OF THE CONSTRUCTION OF SELF-TUNING LOOPS FOR SERVO Sy-_ETCCU) AFB OH

EhhhhEE. AD-Ri FERROMRfGNETIC DIELECTRIC SUBSTRNCE(U) FOREIGN 1/- - - TECHNOLOGY DIV WRIGHT-PATTERSON AFB ON

UNCLASSIFIED AD DEFENSE DOCUMENTATION CENTER FOR SCIENTIFIC AND TECHNICAL INFORMATION CAMERON STATION, ALEXANDRIA, VIRGINIA UNCLASSIFIED

UNCLASSIFIED AD AIMED SERVICES TECHNICAL INFORIATION MGWY ARLINGTON HALL STAION AILINGIM 12, VIRGINIA UNCLASSIFIED

UNCLASSIFIED AD NUMBER LIMITATION CHANGES

FOREIGN TECHNOLOGY DIVISION

TO Approved for public release, distribution unlimited

io -1 i UN LASSIFIED firmed Services echnicall nforma ion Hgency DOCUMENT by SERVICE CENTER KNOTT BUILDING, DAYTON, 2, OHIO Reproduced

UNCLASSIFIED AD DEFENSE DOCUMENTATION CENTER FOR SCIENTIFIC AND TECHNICAL INFORMATION CAMERON STATION. ALEXANDRIA. VIRGINIA UNCLASSIFIED

cot* SEPTEMBER 1965 a CC 0^\ 0 «*«***

SECURITY MARKING. NOTICE: When government or other drawings, specifications or other

ei vices lecnmca Ripriduced ly DOCUMENT SERVICE ßEHTE KHOTT BUIimilt. BUTT»!. 2.

AZIMUTHALLY PROPAGATING MODES IN AN AXIALLY-TRUNCATED, CIRCULAR, COAXIAL WAVEGUIDE

UNCLASSI FILED L10160 DEFENSE DOCUMENTATION CENTER FOR SCIENTIFIC AND TECHNICAL INFORMATION CAMERON STAMTIOI, ALEXANDRIA, VIRGINIA UNCLASSIFIED

QELEC T Ef DTIC. Fit -E. Copy 90! 21., ' FOREIGN TECHNOLOGY DIVISION BEST. AVAILABLE COPY. Ln 00 DEC

INFRCNGCAE ELMNSFR. m E-1525CAT(RN LIKE..(U) AG. FOREIGN WRIGHT-PATTERSON AFB OH 0 S RAYNUS ET AL. e8 APR 85 ENOCN

THE MINIMUM NUMBER OF LINEAR DECISION FUNCTIONS TO IMPLEMENT A DECISION PROCESS DECEMBER H. Joksch D. Liss. Prepared for

AFRL-RW-EG-TM

IEND AD-AI CURRENT DENSIT IN CATHODE SP0TS IN THE CONDENSED

St>-T*-4*-te.» ESD RECORD COPY. ,om*' ESD ACCESSION LIST ESTI Call M - 4H THIRD QUARTERLY TECHNICAL REPORT October to 30 December 1967

DISTRIBUTION STATEMENT A

D " TIC. gforeign TECHNOLOGY DIVISION II 13. Approved for public Telease; Distribution unlimited. THE THIRD GENERATION OF

A GENERALIZED RADAR OUTPUT SIMULATION. J. F. A. Ormsby S. H. Bickel JULY Prepared for

8 9. 7~ FOREIGN TECHNOLOGY DIVISION. Ca Ca 00. JuL ]TD-ID(RS)T THESES MND AMAOTAIONS OF A SCIETIFIC AND TECHNICAL

Foundations of Discrete Mathematics

UNCLASSIFIED AD Reproduced ARMED SERVICES TECHNICAL INFORMATION AGENCY ARLINGTON HALL STATION ARLINGTON 12, VIRGINIA UNCLASSIFIED

UNCLASSIFIED AD luf, the ARMED SERVICES TECHMCAL INFORMATION AGENCY ARLINGTON HALL STATION ARLINGTON 12, VIRGINIA UNCLASSIFIED

UNCLASSIFIED AD p4d4 x ARMED SERVICES TECHNICAL INFORMATION AGENCY ARLINGTON HALL STATION ARLINGTON 12, VIRGINIA UNCLASSIFIED

UNCLASSIFIED AD DEFENSE DOCUMENTATION CENTER FOR SCIENTIFIC AND TECHNICAL INFORMATION CAMERON STATION, ALEXANDRIA. VIRGINIA UNCLASSIFIED

Fluid Mechanics Abdusselam Altunkaynak

fll m L31 12 MICROCOPY RESOLUTION TEST CHART f41l BUREAU OF STAI4DAN A mill

UNCLASSIFIED. AD 401f103 DEFENSE DOCUMENTATION CENTER FOR SCIENTIFIC AND TECHNICAL INFORMATION VIRGINIA CAMERON STATION. ALEXANDRIA.

CONSERVATION OF MASS AND BALANCE OF LINEAR MOMENTUM

IIIIIIIIIII.EE. EIIIIIIIIIIIIu UKIII/lE

REE Internal Fluid Flow Sheet 2 - Solution Fundamentals of Fluid Mechanics

UNCLASSI FIED AD ARMED SERVICES TECHNICAL INFORMI AlIMGTON HALL STATION RLIN 12, VIRGINIA AGENCY UNCLASSIFIED

Geometric interpretation of signals: background

New Uses of Sulfur II

Week 6 Notes, Math 865, Tanveer

REVISIONS SYMBOL DESCRIPTION DATE APPROVAL

G~OO6oWi's ESTIMATING TIMES TO EARLY FAILURES USING SAMPLE DATA TO ESTIMATE THE WEIBULL SCALE PARAMETER AFFDL-TR-77-89

TO Approved for public release, distribution unlimited

U10057 FOREIGN TECHNOLOGY DIVISION. if. AIR FORCE SYSTEMS COMMAND. Fl WRIGHT-PATTERSON AIR FORCE BASE OHIO - 8.

0n Stokes' Problem for a Non-Newtonian Fluid. K. R. Rajagopal, Pittsburgh, Pennsylvania, and T. Y. Na, Dearborn, Michigan. (Received August 30, 1982)

ASYMPTOTIC STRUCTURE FOR SOLUTIONS OF THE NAVIER STOKES EQUATIONS. Tian Ma. Shouhong Wang

UNCLASSIFIED AD DEFENSE DOCUMENTATION CENTER FOR SCIENTIFIC AND TECHNICAL INFORMATION VIRGINIA CAMERON SIATION, ALEXANDRIA.

UNCLASSIFIED AD fh ARMED SERVICES TECHNICAL INFORMATION AGENCY ARLINGTON 12, VIRGINIA UNCLASSIFIED

V (r,t) = i ˆ u( x, y,z,t) + ˆ j v( x, y,z,t) + k ˆ w( x, y, z,t)

UNCLASSIFIED 408F102 DEFENSE DOCUMENTATION CENTER FOR SCIENTIFIC AND TECHNICAL INFORMATION CAMERON STATION. ALEXANDRIA. VIRGINIA UNCLASSIFIED

History of Chemical Engineering

The number of marks is given in brackets [ ] at the end of each question or part question. The total number of marks for this paper is 72.

I RD-fl THE PROXIMITY EFFECTS OF SUPERCONDUCTING MULTILVER /i

Modeling of liquid and gas flows in the horizontal layer with evaporation

UNCLASSIFIED. An QepAaduced. by ike ARMED SERVICES TECHNICAL INFORMATION AGENCY ARLINGTON HALL STATION ARLINGTON 12, VIRGINIA UNCLASSIFIED

A Fundamental Structure of Continuum Mechanics I. Elastic Systems

Chapter 6. Convergence. Probability Theory. Four different convergence concepts. Four different convergence concepts. Convergence in probability

SCATHA/SC3 DATA PROCESSING AND CROSS- CALIBRATION WITH LANL-GEO/CPA FOR AE9 DEVELOPMENT

UNCLASSIFIED. AD 295 1l10 ARMED SERVICES TECHNICAL INFUM ARLINGON HALL SFATION ARLINGFON 12, VIRGINIA AGCY NSO UNCLASSIFIED,

UNCLASSIFIED M 43^208 DEFENSE DOCUMENTATION CENTER FOR SCIENTIFIC AND TECHNICAL INFORMATION CAMERON STATION. ALEXANDRIA. VIRGINIA UNCLASSIFIED

Ascorbic Acid: Chemistry, Metabolism, and Uses

UNCLASSIFIED AD ;1 DEFENSE DOCUMENTATION CENTER TECHNICAL INFORMATION SCIENTIFIC AND CAMERON STATION, ALEXANDRIA, VIRGINIA UNCLASSIFIED

Technical Note

Sequences. We know that the functions can be defined on any subsets of R. As the set of positive integers

arxiv: v1 [math.gm] 2 Jun 2018

UNCLASSI FlED. 8oei, DEFENSE DOCUMENTATION CENTER FOR SCIENTIFIC AND TECHNICAL INFORMATION CAMERON STATION. ALEXANDRIA. VIRGINIA UNCLASSIFIED

Laminar Boundary Layers. Answers to problem sheet 1: Navier-Stokes equations

This article appeared in a journal published by Elsevier. The attached copy is furnished to the author for internal non-commercial research and

Convective Heat and Mass Transfer Prof. A. W. Date Department of Mechanical Engineering Indian Institute of Technology, Bombay

Solutions to Assignment 3

UNCLASSIFIED UNCLASSIFIED DEFENSE DOCUMENTATION CENTER SCIENTIFK AND TECHNICAL INFORMATION FOR CAMEROW STATION, ALEXANDRIA, VIRGINIA

Transcription:

UNCLASSIFIED AD 295.796 ARMED SERICES TECHNICAL INFORMATION AGENCY ARLINGTON HALL STATION ARLINGTON 12, IRGINIA UNCLASSIFIED

NOTICE: When government or other drawings, specifications or other data are used for any purpose other than in connection with a definitely related government procurement operation, the U. S. Government thereby incurs no responsibility, nor any obligation whatsoever; and the fact that the Government may have formulated, furnished, or in any way supplied the said drawings, specifications, or other data is not to be regarded by implication or otherwise as in any manner licensing the holder or any other person or corporation, or conveying any rights or permission to manufacture, use or sell any patented invention that may in any way be related thereto.

29 457 9 ASTIA rc7.l1 ON THE SOLENESS OF SOLUTION OF BASIC PROBLEM CONCERNING FREE THERMAl, CONEC(TION OF LIQUID By uisia B I. 0. Sevralk 295 796 r

ID-TT-62-1613i1 1 UNEDITED ROUGH DRAFT TRANSLATION ON THE SOLENESS OF SOLUTION OF BASIC PROBLEM CONCERNING FREE THERMAL CONECTION OF LIQUID BY: I. G. Sevruk English Pages: 6 SOURCE: Russian Periodical, Izvestiya ysshikh Uchebnykh Zavedeniy, Matematika (Kazan), Nr. 4, 1958, pp. 218-221 s/140-58-0-4-l THIS TRANSLATION IS A RENDITION OF THE ORIGI. NAL FOREIGN TEXT WITHOUT ANY ANALYTICAL OR EDITORIAL COMMENT. STATEMENTS OR THEORIES PREPARED BY: ADOCATED OR IMPLIED ARE THOSE OF THE SOURCE AND DO NOT NECESSARILY REFLECT THE POSITION TRANSLATION SERICES BRANCH OR OPINION OF THE FOREIGN TECHNOLOGY DI. FOREIGN TECHNOLOGY DIISION ISION. WP-AFB, OHIO. FTD-TT- 62-1613/1 Date 18 Jan 1963 B

On the Soleness of Solution of Basic Problem concerning Free hermal Convection of Liquid. by I* GSevruk 1 Assuming that in a certain volume, limited by a closed surface S is situated in state of thermal convective movement a viscous, mechanically incompressible liquids and assumng that on the boundary of the zone and at the initial moment of tim is given the distribution of velocity and temperature of the liquid. It is necessary to find the distribution of them values by the volume of the liquid at a given mmnt of time, Assuming the existence of a solution for the mentioned problem, we will ove its soleness, For this we employ the D*Ye*Dolidzell] method. Equations of free thermal convectior have the form of [2] 3 Squatins offreet a T-- ( vvt) = ZAT, ) dt l div v =-0, IjO where v- velocity of the liquid, p-read from hydrostatic pressure of the liquid, T6 temperature of the liquid, read from a certain constant mean value TO, (TO). density of the liquid, g-gravity acceleration,*-,, y - coefficients of kinenstie viscosity of thermal expansion and heat conduction of the liquid. The sought for values should satisfy the given conditionsa o-- (r), To =,(r)

(the sign a designates the boundary, and 0 - the initial value of corresponding value ). 29 We will assume, that there are two solutions for problem (1) - (5)s Then functions (, PI, T) H (,, P2, T). (.) U,-, q =pi-p ' o-t-t2 T2 will satisfy equations Ot au + o + () 2+ { r ) -A - 7 at+ vo+ ut2 divu = 0(..q and conditionsa U,--o0, es --o, jo UO=O, O O- To prove the theory of soleness it is necessary to, show that u = 0 and 0 P 0. For this purpose equation (7) is nmltiplied scalarly by u, equation (8)-by 0 we will combine same and then integate by the volume of liquid; we will obtain J'(u + o8) d'+flu(vlv)u+o(viv)od+fu(uq)v ' 2 d= =-fui-dv+f(ua+oao)d-f Ou(?g+ T 2 )d.(') P f Taking into consideration the continuum equal;ion and the boundary values of the functions u and (9, we transform the integrals included in (12) with the- aid of the Gauu-Ostrogradskiy and Grin formulas. In consequence we will obtain T-TT-62-i613/i 2

f UdTU dt / dt 2 2 d t v fp1u ±O(+0(iv) dp(,17)(u+ L) d= 1 Jdlv Iv, (U2 + 61)J d= 0, fv, q d- fdiv zi d-o, J'(UtU + YomO) d - f v (rot u) 2 + y (grad 0)' d. 710

Sabstituting the found values of integrals in (12) we will obtain d= -2 fv(rot g)' +(grad)d- 2 (,) v. 2 d - - 2 Jou(Sg+vT.,)d. Since v, y> 0, then the first ccmponent of the right part (14) is negtive and, consequently d 2fu (uv) 2d -2f (U 4T 2 W. v In the initial moment of time the function K(t) equals zero, and further on it /-be natia. Consequently in a certain interval of time 0( t - T dk - >' 0. In such a case, by ccuparing the absolute values of left and right parts of the inequality (15) for 04- t 4 -Z we obtain d<<2fu (U) 2 d + 2 fou(pg+t 2 )dj Evaluating the -ngnitude of the integrals, included in (16), we obtain fu(u)ad1'mfu~d<mk, where M - mean value 5 g) (1 - crosscut of direction u); fou(pg± T 2 )d ANflOluld,<Nf(U2 +63)d=.'-N.K, f ---_2 where N - mean value \ l * Taking into consideration the obtained evaluations, we will have f or 0 = t 4-- - I where A n 2M * No al 04 It is apparent, that the most rapid changes in function K with time in the inter- will be determined by condition dk. A K, LT dt i.eowhen K = conat.exp, Adto Henceconsidering (11) and (13) we obtain for 0 t I K a 0 and consequamtly FTh-TT-U-1613/1 3

Next we. will do as follows, We will break up the values t >0 into two classes, To the first class we will refer all t of the interval 0/ t ',. for which K = 0. The remaining t, for which K + 0, it is assumed are forming the second class. It is apparentothat the first class is net emptye Such a breakdown, according to the Dedekind theorem, is justified and is done by the number -, which appears to be maximm in first class. In such an instance for all tl*( 9 K(t)a0 and for any jexist such t o, 0 &. to-.t _ for which K(t') 0. On the other hand, it is evident from the proven facts with consideration of the continuity of function K(t) and condition K(') - 0, that for, a certain E 1 and all to satisfying inequality 0 Z t - U lok(t) = 0, which contradicts the made assumption. Consequeatly all values t are included in the first class and therefoe u O 0H0 O ;ka Bcex t>o. (1/7.) Aa to the pressure then as shown by equation (7) it is possible to synonymously determire he pressure gradient only. 3e The mentioned in point 2 proof of the soleness theory in the solution of the basic internal problem of free thermal convection of liquid can also be expanded for tk case of an external problem~kj. This can be realized by an ordinary maximum transition from the finite zone into the infinite, requiring the fulfillment of conditions of dampint at infinity8 L where alpha > 2, r - I r1+av J' Ir1+QT JI Ir'pl, Ir'+9rotvtI, Jrt+-gradT J- O (17c 1 ) (i=-1, 2), distance from a certain aasumed as origin of coordinates, point of heater. The author expresses thanks to B"1eGagyev and S.3,ihl'nk for the valuable information and a number, of critical notes. Su.mitted Febr.e819J8a m-t'-62-1613/i 4

The A.Mofo.Gkiy Form State Universi1ty Iiteratur., 1. D*Ye*Dlidze* Dolady Akadeuii Nauk SSM1, vol.96,no.39 1954 2. L.DLandau and Ye*M.Lifshitse Mchanics of Continuous bnidiaqgittl1954 FTD-TT-62-163A/ 5

DISTRIBUTION LIST DZA~il OF DEMINSE Fir. Copies Y-AJOR AIR CMZ'A',S Nr. Copies fli'adqu.,itzrs USAF AiFSC SCFT-12. ASTIA TD-231a 25 5 AFCI:T-D TD-Blb 3 1. ADC (ADY) 1 (A3.SSn 1s~ (ssf) 2 AFFTC (FTY) AJ'BWC (SWF1 OTH91R AGENCES NASA1 RAIM - 2 2 2 -.- i-62-1613/1 6