SCIENTIFIC ABSTRACT MOUREK, J. - MOVCHAN, B. A.

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SCIENTIFIC ABSTRACT
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TRAVNICKOVA, E.; MOURSK, L.:,TROJAN, S. The effect of repeated blood losses on resistance to nitrogen and stagnation anoxia during postnatal development of the rat. Physiol. babowslov. 11 no.3:231-235 162. 1. Institute of Physiology, Faculty of General Medicine, Charles Uni- versity, Prague. (HEMORRHAGE experimental) (NITROGEN pharmacology) (ANOXIA experimental) MOUREK, J. Oxidative metabolim, its development and Influence in the ontogenesis of mammals. Sborn. lek. 64 no.5:136-144 My 162. 1. Fyziologicky ustav fakulty vasobsonsho lekarstvi University Karlovy v Praze, prednosta prof. dr. F. Karasek, DrSc. (CERML MMM SYSM metabolism) (OXYGEN metabolism) (STARVATION exper) (AGING pbysiol) MOUREK, J. Development of oxygen requirement in ontogenesis in the dog. Sborn. lok. 64 no.lOs3l6-320 0 162. 1. Fyziologicky ustav fakulty vseobeeneho lekarstvi University Karlovy v Praze prednosta prof. dr. F. Karasek. WIMAW NEWBORN) (TISSUE METABOLISM) MOUREK, Jindrich Fasinination of metabolic relations during the course of ontogenesis vith the aid of anzymtic Inhibitors. Cas. lek. cesk. 101 no.29/302 918-922 20 J1 162. 1. Fyziologicky ustav fakulty vseobeeneho lekarstvi KTJ v Praze, pred- nosta Prof. dr. F. Karasek, DrSc. (TISSUE METABOLISM pharmacol) (MALONATES pharmacol) MOUREK, J. The effect of 2: / din-i trophenol on oxygen conitopti cn and res ~s tanc ~ to nitrogen anoxia during the dev,~-.lopnent of tr.e rat. Physic-', bohemoslov 12 no.1:70-75 16-11 I.Institutti of Physiology, Faculty of Medicine, Gharles UnIversity, Frague. (111TROPH11101,S) (141TROG111) (ANOXIA) (TISSUE f-J-SPIRATION) (GROWTH) (ANIMALS , NEWBO'101) MOUREKI-'~~, The effect of hypoxia on oxygen consumption of cerebral cortex, liver slices and of diaphragm in vitro during postnatal development of the rat. Phyaiol. Bohemoslov. 12 n0-42377-381 163o 1. Institute of Physiology, Faculty of General Hadicine, Charles University Prague. 4NOXIA) (CEREBRAL CORTEX) (LIM) (MUSCLES) (TISSUE METABOLISM) (GROWTH) (MANOMETRY) (DIAPHRAGM) MOUREKY Jj- PELISKOVA, M. 2,,4-,Dinitrophanol and its action in the ontogenesis of rats. (LD50 of 2,,4- t (t E T), is a process toc. 1.3 There exists a process z . z (t) defiAed on the total interval T and which is denoted as undisturbed process. Card 1/4 $8749 S/040/60/024/006/003/024 a ill/ C 333 Stability of Processes With Respect to two Metrics If z belongs to a Process in the moment t, then it is said that the pair (Z,t) belongs to the process. To every pair (z,t) there are defined two metrics (distances) S o(z, t), 3 (z, t) with the properties t 2.1 so(z,t) is real nonnegative, where 3 0(zo(t),t) =- 0, t e T. 2. 2 3 (z, t) is real nonnegative, where 3 (z0 (t), t) ~ 0, t e- T. 2.3 The distance 34z,t) is continuous with respect to the metric g O(z,t) EuniformlyJ on T !:-~ T, i. e. to every E > 0 and toe T 0 there exists a gof- 1t0) 71 o EJ(E) > ol so that 5 (z,t0 < 6 is satisfied for all (z,t 0) for which 30(z,to) < 2.4 For every process z(z 0, top t) defined on (t 0 , t00), 3(Z(Z0 t0, t), t) is continuous in t (here 5(z(zol top Opt) is the distance from the undisturbed process up to the point z of the process z(z,, t 0 , t) in the moment t. Card 2/ 4 88749 B/040/60/024/006/003/024 C ill/ C 333 Stability of Processes With Respect to two Metrics Theorem 5-1: In order that the undisturbed process zo(t) on T be stable with respect to the me-trios SO'l , where the initial moment t0belongs to T'5;i T, it is necepsary and sufficient that there is an R N 0 so th1t on RZT there exists a functional f(z,t) positive- definite in the metric I and non-increasing which is continuous on T0 in the metric to. Theorem 5.2 is an analogous statement for uniformly stable processes. Theorem 6.1 is a generalization of the theorem of instability of Chetayev (Ref.2) to the case of two metrics. There are 14 references: 13 Soviet and 1 Japanese. SUBMITTED: July 14, 1960 Card A14 MOVCHAN -A A 11-00C PHYS-MATH SCII "PROBLEMS OF STABILITY I ~ OF THE DEFORMATION-V~ ~ Of SOLIDS." MOSCOw, 1961. (MOSCOW URDER OF LENIN AND URGER OF LABOR RED BANNER STATE UNIVERSITY OMEN# M. V, LOMONOSOV). (KL-OV, 11-61, 207). -1- M"CHA"T, A. A. "Running Wa,res in the Problem of Hypersonic Flutter of Panels of Finite length. 0 Paper presented at theThird International Congress in the Aeronautical Sciences, Stockholm, 27-31 August 1962 IIOVCWT, A.A. (Moscow) "The analogue of Kelvin theorem on the conservation of stability with the addition of dissipative and gyroscipic forces for the case of arbitrary displace-ments; xid deformations of solids". report presented at the 2nd All-Union Congress on iheoretical and Applied Mechanics, Moscowp 29 Jan - Feb 64. ~r, HO ACCESSION NR: AT4039439 S/2879/64/000/000/0695/0701 AUTHOR: Movehan, A. L (Moscow); Movchan A A (Moscow) TITLE: Vibration forms in the problem of supersonic panel flutter SOURCE: Vsesoyuznaya konfereniiiya po teoril obolochek i plastin. 4th, Yerevan, 1962. Teoriya obolochek i plastin (Theory of plates and films); trudy* konferentaff, 19G4, 695-701 TOPIC TAG: panel, panel flutter, wave propagation, supersonic- flutter, panel vibration, gas flow, supersonic gas flow, flexure, damping, boundary problem. ABSTRACT: Noting that the use of high-speed digital computers makes it possible to discover. the characteristic peculiarities of the eigenforms of the vibrations of panels within a super- sonic gas flow, the authors present several such peculiarities which are common to panels of different configuraUons in a plane. For simplicity of exposition, the discussion in based on'. the simple equation J*W P.X dw dw N D dt* er &C where w(x, t) Is the flexure of tbe'panel, occupying a region in We form of a band x4 0c; Lcard 1/6 od 0,0 0A 00 alp Ole v0. el, ty, '%e 0 SO. aes ~Cjlb~&IA* 000' 0 to co ova 0,00 -4e OW, 0oci \Voon~o~, o-% ~AXNo op - VO %P :v -le tot se t 'o X 3s!N' e,\.1 6."0 060 - I r0) 0t ,deS "PI, 19 VP* o O~ Ivi eolo -.0 ~trj, 40"- e, CV .Pot ~ OP $6, Sv I lcdw %e %V 00 COS S-oo 00 W" ot N, V)e4l 44 CNIN g~6 JA~ 'ID . 0- ACCESSION NR: AT4039439 The dimensionless values x W V, ID (4) ,are introduced in the solution of Eq. 1. Perturbed movements of a panel yield the form. W (X, 1) X (X) e (5) Function X (x), appearing In Eq. 5, is the eigenfunction (~on-trtviai solution) of the boundary 'Problem L4X - A xx, d~e dx (6) 1 1. V. L 4. Lf (X) ,where Li(X) indicate linear homogeneous boundary conditions at the edps x0, x1. For Card -3/6 'ACCEssioN NR: AT4039439 !the determ'ination of the eigenfunctions there is derived the following equation L, (A') L, L.- (XJ) L, (X4) F (A, X) so L, (XI') L, (XI) L, (X2) L, (XI) .0, (7) La (XI) L, (XI) L- (XI) L, (P) L, (XI) L4 (XI) L: (P) Lj (XI) ,the left-hand part of which is the whole analytical function of parameters A, To each root ': A of this equation there corresponds, at least, one solution Cj of system 11 and eigenfunction !10. If the eigenvalue A ia a simple root, one (with accuracy W constant factor) eigenfactor ,X(x) corresponds to it. If the eigenvalue X Is a double root and the rank of matrix 12 equals two, two linearly Independent eigenfunctions correspond to it; if the matrix rank equals three' ,only one eigenfunction X(x) corresponds to eigenvalue ArW eigenfunction X(x).9f the ;boundary problem can be presented In the form (8) + I" !ACCESSION NR: AT4039439 where XI(x), X2(x) are real functions. It Is found that the natural vibrations are described by the formulas I X W I Cos It W + A 60 - W ~X, t) X (A) I sin I? (X) + q11 do, (9) For a real eigenfunction X(X) in continuity intervals 4) (k) condition V (k) constant is ful- filled, thus providing a basis for calling the natural vibrations in this case standing waves. It is shown that natural vibrations in the form of traveling waves. (for a complex eigenfunction X(x) in continuity intervals V (x) with fulfillment of condition V (x) j const by analogy with j equation (92)) are a typical phenomenon in the case of panel flutter. A theoretical qualitative' investigation of the character of the traveUng waves in flutter, formerly involving extremely cumbersome computations, has been facilitated through the use of high-speed computers. The process of finding the eigenfunctions X(x) Consists primarily in the solution of rather complex transcendental equations with respect to the parameters (r, 0 (which are complex numbers for complex and In subsequent computation. In the final section of the article, the computation resultar achieved on a "Strela!' computer, for the vibrations of an edge- jammed pawl (x - 0, x - 1) are given and discussed. Orig. art. has: 4 figures and 21 formulas., ,-Cord.5/6_ F [ACCESSION NR: AT403"39 ASSOCIATION: none SUBMrrTED: 00 DATE ACQ; 14May64 ENCL: 00 SUB CODE: AS NO REP SOV: 006 OTHER: 001 ACCESSION NR: AT4039439 S/2879/64/000/000/0696/0701 AUTHOR: Movch L (Moscow); Movchan, A. A. (Moscow) TULE: Vibration forms in the problem of supersonic panel flutter SOURCE: Vsesoyuznaya konferentelya po teorii obolochek i plastin. 4th, Yerevan, 1962. Teoriya abolochok i plastin (Theory of plates and films); trudy* konferentaii, 1964, 695-701 TOPIC TAG: panel, panel flutter, wave propagation, supersonic, flutter, panel vibration, gas flow, supersonic gas flow, flexure, damping, boundary problem ABSTRACT: Noting that the use of high-speed digital computers makes it possible to discover. the characteristic peculiarities of the eigenforms of the vibrations of panels within a super- sonic gas flow, the authors present several such peculiarities which are common to panels of different configurations in a plane. For simplicity of exposition, the discussion Is based on- the simple equation &W A0, dw dw D t 1. 2- " -a where w(x, is the flexure of the'panel, occupying a regton in the form of a band 0.~f x,,6 4%; Lcard 1/6 r ACCESSION NR: AT4039439 I E is a dimensionless number indicating by how many times the full external damping exceeds the aerodynamic damping, as calculated by the well-known formula of the piston theory (A. A. 111yushin. Zakon ploskikh secherdy v aerodinamike bollshikh averkhzvukovykh skorostey. PMM, 1956, 20, no. 6), while the other nomenclature coincides with that given in A. A. Movchan (Ob ustoychivosti paneli, dvizhushcheysya v gaze. PMM, 1957, 21, no. 2). (a panel moving in a gas in the direction of the positive axis x). The solutions of Eq.' 1, which satisfy the boundary conditions at the edges x = 0, x = a, are compared with mcno- chromatic waves of length a I n 2x)y-L rfW1,, (x~ i) - sin LX+ [a which satisfy Eq. 1 without the right-hand part and derived without allowance for the boundary conditions at the edges x 0, x a. The propagation velocity of the waves (Eq. 2) is given by the formula- 2* (3) 2/6 7 ~ACCESSION NR.--A---T'4039439 The dimensionless values x pa4 (4) Rre introduced in the solution of Eq. 1. Perturbed movements of a panel yield the form, w (x, i)'= x (X) (5) iFunction X (k), appearing in Eq. 6, is the eigenfunction (non-trivial solution) of the boundary problem d4X dX A dx (6) Lf (X) 4. Where IaiM indicate linear homogeneous boundary conditions at the edges x 0, x 1. For 3/6 600CESSION NR: AT4039439 e determination of the eigenfunctions there is derived the following equation L, (P) L, (XI) L, (P) F (A. k)w L, (XI) L, (XI) Ll (XI) Ll (XI) _0' (7) La (XI) La (XI) L (Xs) L, (X4) L4 (XI) L, (XI) L: (XI) La (XI) ~e left-hand part of which is the whole analytical function of parameters A, )L To each root A of this equation there corresponds, at least, one solution Cj of system 11 and eigenfunction 0. If the eigenvalue A is a simple root, one (with accuracy to constant factor) eigenfactor '(x) corresponds to it. If the eigenvalue X Is a double root and the rank of matrix 12 equals Aro, two linearly independent eigenfunctions correspond to it; If the matrix rank equals three,' nly one eigenfunction X(x) corresponds to eigenvalue AzW eigenfunction X(x).gf the oundary problem can be prmented In the form + I., IACCESSIONNR: where X1(x), X2(x) are real functions. by the formulas It Is found that the natural vibrations are described W (V, t) X (X) I Cos It (X) + qtJ CO. W .(x, t) - I X (x) I sin 1~ (ic) + qt] 011 (9) For a real eigenfunction X(x) in continuity intervals 4) (x) condition V (x) --t constant is f al- filled, thus providing a basis for calling the natural vibrations in this case standing waves. It is shown that natural vibrations in the form of traveling waves. (for a complex eigenftnction X(x) in continuity intervals V (x) with fulfillment of condition V (x) ~ const by analogy with , equation (2)) are a typical phenomenon in the case of panel flutter. A theoretical qualitative' investigation of the character of the traveling waves in flutter, formerly involving extremely cumbersome computations, has been facilitated through the use of high-speed computers. The process of finding the eigenfunctions X(x) consists primarily in the solution of rather complex transcendental equations with respect to the parameters aC, P (which are complex numbers for complex \ ) and in subsequent computation. In the final section of the article the computation results, achieved on a "Strelall computer, for the vibrations of an edge- jammed panel (k 0, x - 1) are given and discussed. Orig. art. has: 4 figures and 2jL formulas.. LCard- 5 ACCESSION NR: AT4039439 ASSOCIATION: none SUBMITTED: 00 SUB CODE: AS L"M --- ?10 DATE ACQ-. 14May64 NO REF gov: 006 ENCL: 00 OTHER: 001 MOVCHAN, A.F. Some types of polyclinical aid for thl rural population. Mad. sestra 20 no.7:23-27 JI 161. (MIRA WIC" 1. Zamestitell glavnogo vracha Kiyevskol oblastnoy bollnitsy. (PUBLIC HEALTH, RURAL) MOVCHANY A.P. (Juyev) Hospital nurse. Had. sestra 22 no.6:206-21 Je'63- (MIRA 16:9) (NURSES AND NURSIBG) AUTIIORS~: 11olle-ri V, V, ana Movc~ian A. T. TI'PLE: 'I"ethoets of Decreasin~- the Ash Content in Pitr-'-- U (Puti snizheniya zol'nosti pekovogo koksa) .!;ZRIODICAL: Koks i Khimiya, 1958, Nr E., PP 1?-"Il (UWMI~ ABSTRACT: The influence of various operatin6 factors oi., cl,.;2 a,~" content of tar and tar-pitch is discus-,od --rL by data on the ash content of tar, piLch and pitc.h coi: produced on the Zaporozhsk coke oven vjorI:s (Tables 1, The influence of tY,,,, followinb operatinf, factorc is mentioned: 1) charfJ.nE conditions of co':e oven, the degree of finenesc of the coal blend and thc and duration of stuam injections; 2) condition of operation of tar settling: tanks, intermediate aiid, stora, i tanks and 3) additions of soda to tar before d_*._--I_-,I1--ti,_. V:ere are 2 tabl~ac ~~nd. 1 ZnIx~roz,-EIrly zavrxi rr,-,.I.'.-e Coal-tar Chezdcal PlanLi i. Ovens--Performance 2 Coke--Combustion 3. Fue1s--Prc:-,)erti_e~-) Z2 r~! 1 / 1 KULESHOV, P.Ta., kand.tekhn.nauk; MOVCHAS, A.T. New system of processing the anthracene fraction. loks i khim. no.q: 36-37 160. (MIRA 13:9) 1. Zaporozhakiy koksokhimicheeldy zavod, (Anthracens) MOVCH M,-~- Adoption of modern equipment and technology. Koks 5-9 163. (Zaporozhlye--Coke industry) khim. no-5: OIIRA 160) MOVCHAN .4 V.F.; LIVSHITS, B.Ya.; BUTUZOV, H.D. - I A.T.; POPOV, K.P.; SOKOLGIi Automation of sulfate recovery plants. Koks i khim. no-5:39-43 163. (Coke industry-By-products) (Automation) (MIRA 16:5) KASATKII:, B. S. , -'IMCEMN, B. A. Steel Alloys Some data on the infl,uence of a metastable structure on the mechanic-tl pr(, erties (.f metal. Avt(-m. svar., 4, No. 6 (21), 1951. Monthl-v ILs_t 2L Russian Accessions, Library -f Congress, June 1952. Unclassified. MOVCHAN, B. A. Movehan, B. A. -- "Some Properties of Primary Crystallization in Automatic "Ilding of Alloy Steel." GandTech Sci, Inst of Electric Welding, Acad Sci Ukrainian SSR, Kiev 1953. (Ref era tivrWy-rhu -rnal--Xhimiya, No 1, Jan 54T- So: SUM 166) 22 July 1M KOTC11a, B.A. Some characteristics of the primary crystallization process of alloy steel. Avton.evar.6 no.3:3-15 NY-Je 153. (MMA 7:5) 1. Institut elektroevarkI im. Te.O.Patona Akadeall nauk USSR. (steel alloys) MOW@ Aa,?, AD.It-. ussElphysics - alloy steel grains FD-1074 Card 1/1 Pub. 153 - 10/24 Author Svechnikov, V. N., and Movehan, B. Title : Structure of the primary grains of alloy steels during heating to a high temperature (i3oo-14oo0c) Periodical : Zhur. tekh. fiz., 24, No 10, 1823-1829, Oct 1954 Abstract : The authors study by direct methods the structure of the grains and the boundary zones of several alloy steels (results tabulated), namely at temperatures of overheating. They find that chromium and wolfram diffuse into the boundary zones of the grains and that man ese may concentrate at internal defects because of rolling. They describe their experimental procedures and evaluate their results. Institution : - Submitted : January 29, 1954 PARKOVSKIY. Yevpniy Adamovich; KOVCHAN. Boris Alsksoyevich; STITSINKO, TwevDlod Ivenovich; SAEV1fjLUV,' T..Vvedushchly rodalctor; MOVIX, A., tokkmichookiy rodaktor Lladioinotopes in metal reaearchl Radioaktivuye isotopy pri tooledo- vanii metallov. Kiev, Goo. izd-vo takhn. lit-ry MSR. 1956. 87 p. MaA 9:10) (Radioisotopes--Industrial applications) (Ketals) AM P - 5254 Subject USSR/Engineering Card 1/1 Pub. 11 - 5/15 Authors Gupalo, Yu. D., B. A. Movchan, and P. M. ShIrokovskiy (Electrowelding lnstitute~'-Iml ~.' Paton) Title Use of radioactive Isotopes to control the level of metal melt in the resistance slag welding vat. Periodical Avtom. svar,, 4, 67-69, Ap 1956 Abstract The authors describe the utilization of radioactive isotopes for control of level of melting metal In the vat of resistance slag welding. A special automatic regulator was designed and tested by the Electrowelding Institute Im, Paton, Two drawings; 3 Russian references (1953-55). Institution As above Submitted No date SrACHNIKOV, V.N*; HOTCHAN, BoA. . Nquilibrium of chemical inhoagensity In allo7s at high temperature. Sboy-. nauch. rab. Inst. metallofiz. AN USSR no.7.132-47 156. (Metals at high te"raturoj) (MIRA 11:1) (Ketallography)