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TASHINA? R.S.; GIRZE2261.I Checking an the use of O.P. Mehra, and M.L. Jackeon's method of the removal of iron arid*s from Boils and clays for mineralogical purposes. Kora vyvatr. no.5:398-403 163. (MIRA 16:7) 1. Institut geologii rudnykh meatorozhdeniy, petrografii, mineralogii i gookhimli AN SSSR. (Mineralogical chemistry) GINZBURGI. 1. 1, Remarks on the upper zone of weathering ourfae. Kora. vyvetr. no.5t374-379 163. (MIM 16:7) 1. Institut goologii nidnykh mmstorozhd,~nlv, petrografii, mineralogil 1 gookhimii AN SSSR. (Weatherl-n?) GINZBUPGP I.J.; ANDRUSHCEENKO, P.F. . I Some results of the conference on the comj.(,-)sjt,,nn of witallogen3c and forecasting maps of supergene nir~-' deposits, Korn vyvetr. no.6%312-318 163, Z~.", r.,q) w 1 1. Institut geologii rudnykh meatoro~I*n y, petrografii, mineralogii i geokbimii AN SSSR, Mcsk,,a. GiNnum", I.I. Frag-mants of raminscances. Ooh.po ist.gool.usin. no.l1s46-49 16). (MIRA 160) (Varnadnkli, Vladimir Ivanovich, 1863-1945) T - GIMBURG, ..4 Karst and ze formation. Tz-udy MOEP l2r.116-53 164 - (min 188,k) GIVZBURG, I.M.,, inzh, Automatic control of the load on a scraper motor. Mekh. stroi. 18 no.Utl7-18 N 161. (KIRA 16:7) (Scrapers) (Automatic control) USSR/Phjsif'_-al Chemistry Moiecule, Chemical Bond. B-4 Abs J,-,Lir Referat Zhur - KlimLya, No 1, 195'(, 1111 Author Ye.F. Gross, I.M. Ginzburl-. Inst Title Sl,el,tru of Uomnos Lte S.,atterin[, Df Crysta~ f M e -ular Compounds. Orig Pub Optika i spektroskopiya, 1956, 1, No 5, 710-714 Abstract With a view to investioate the influence of the formation of molecular compounds on spectra, the spectra of monocrys- tals SbCl (1) and SbBrj (II) were studied. Low frequen- cies of On cm-1) 35, 50, 66, 96 and 63 and frequencies of intramoiecukaL oscillations (IMO) of 133, 152, 317, 342 for I and 92, 110, 227 and 236 for If were foup4. The mi- nimpm and maximum moments of inertia (Ix . 10-40 and 10-40 g x of the molecules of I and II are: IY - Ix = 303 and 696, 1 y " 523 and 1210. The low frequencies are satisfying the relation 2 2 Card 1/3 1 / 2 ~: 12/ Il (1) valid USSR/Physical Chemistry Molecule, Chemical Bond. B-4 Abs Jour Ref Zhur Xhimiya, No 1, 1958, 14l for the frequencies of the rotational oscillations in iso- morphous crystals. The low and the M frequencies of 2SbC1 3- CA (III) and 2SbBr 3-C6H6 (IV) are as follows: 22, 43, 64, 83, 110, 117 (111); 22, 42, 58, 71 (IV); and 136, 162, 312, 327, 350, W6, 989, 1176, 1573, 1607, 3062 (111); 69, 102, 213, 225, 241, 990, 3o65 (IV)- The comparison of the spectra of I, II, III and IV leads to the conclusion that the low frequency spectra of I, II and III, IV differ essentially, while the DIO frequencies of III, IV coincide with the D40 frequencies of I, II and C6116- Consequently, the molecules of I, II and C6H6 move in lattices as a whole with reference of one to another. The frequencies 22 and 42 - 43 of III and IV refer to the rotational oscillations of C H6 The frequencies 64, 83, 110 (111) and 42, 58, 70 (IVI s;tisfy (1) and correspond to the rotational oscillations of the molecules of I and Card 2/3 . USSR/Physical Chemistry - Moiecule, Chemical Bond. B-4 Abs Joux : Bef Zhur - Khimiya, N,) 1, 1958, 141 II located in approximate1y equal for~!e fiel(is. Card 3/3 YALIT30VI A.V.~, GINZ111111G, I.Y. 34 Derl.vallwin of imidazole. Part 34. &ur. fit. kntm, - n,-,). 5 1 ( 141 ft A17 t 7 ) 1624-1633 MY '6'0. 1 T ik j:1 I WOO i/65/000/004/6029/DO291 :AO so 44' Fiz 'Tiluv I ti 0 the 44 4 troOk NW*49:19645 167 CI mid Ob.' *ado;daWounds acetic acid, eaters epee- t. 139 ~if;jjhUomeetie acid-eater system are studied. ~60 tii toi: i4s show a band for undisturbed CzO oa 06 Oise` $14, -v film lotion; i e*t whichVeorr"pono to acid dimerso This show atom in the carbmyl and oiko at the go, fom 0 11 v oxygen M dicals t1kii le 440 0 a61d*,1a;1785 ci-I band vhich corresponds tc a a with bands for free and bound C~rbonyl' rad J~ 0q4te the ioiA, cirbonyl band. It is concluded that the: Molecule 0 n band only with one wlecule of or; fo*. a 4~; aim be 6culso Yu. Kissin. ...... ....... (.; , i . j., I ". . .1 .. I... .... t . ;-C, : ~ 1.: 11 ~ 1 4 GTIlZBORG ~ U.I..; PEMV., EA. i SHAM":SHTE'j7l'., A.I. ,,-CoTap,tr'~c,n of tho tqle-!fvm~lonor proper'is!j of* the series ot' a!-I'phat]" wid y 1.1,1, -,'h!-:.i dUT:MP interatAicin with CH .30D. ~Zhur-. cb. ldv:n. '44 31 1 (MIRA .1--, %8) GINZBURG, I.M.; LOGINOVA, L.A. Spoctroscopic manifestations and energy of the intxwnolocular hydrogen bonding in thiosalicylic acid. Dokl. AN SSSh 156 no. 6tl382-1385 J9 164. (MIRA 17:8) 1. Laniagradskiy khimiko-farmatsevticheskly institut. Prodstavleno alcademikom A.N. Tereniym. GINZBURGI I. P. "On the Question of the Notion of Real Gases at High Velocities," Ucheniye Zapiski IAU, No.42, pp. 5-6o, 1939 Dissertation for the degree of Oachelor of Physico-Mathematical Sciences. Presented in December 1937, 4f I . 0. '~Iz " 0 90P.3TSKITA, B. A., OZII'P,(YV'o A. I., 11"NFLCTA, A. N. ?-. USSq (600) 4& Manganese Ores - Polwochnoye Deposits 7. Study of the composition of the manganese ores of the Polurochnoye deposit. (Abstract.) Izv. Glav. upr. geol. fon. no. 2. 1947. 9. Y-ont)-ly List of Ruspian Accessions, Library of Congr-ss, Mar-ch 1953. Unclassified. GINZBURG, I.P. Sufficient yf+py?+qy stability conditions for the solution of m 0. Uch.%& 149* (Iquations, Theory of) the epation; (MIRA 10:3) C,INZBM, I.P. ............. ~ Jkplations for the motion of Tariable-mass eollds. n0.114:205-.216 149* KU 1013; (motion) UBM /Physics Hydraulic impact Jun 52 "Co=putation of Hydraulic IvA;act in Pipes With Variable Cross Section," D. M. Volkov, I. P. Gimm- burg Vest Leningrad U. 54er Mmt, Fiz, Xhim, Vol 7, so 6-. pp 29-46 Gene=lizes results by 1. F. Livurdov (Iz Artill AksA imeni Dzerzhinskogo, 18 (1944)) for the cam the" vall thickness of pipe and souiA velocity- varlAbles, and presents solutions of problem f4w -vL vide class of pipes vith v iable cross sections. 25=100 GZ= On sufficient stability conditions of zero solutions for a-order linear homogeneous differential equations and n-homogeneous differential equation systems with variable coefficients. Veot.Len.un.9 no.5:53-65 MY '54. (Differential equations) (KLRk 9--7) GISHM, I.P.; GRIB, A.A. f~ Water hammer In a complex conduits. Yeet*Len.un. 9 no.8:107-128 Ag 154. Veet.Ien.un. 9 no.8:107-128 Ag 154. MR& 8:7) (Water hammer) tN lip. ,I L E . .... i 1; J,:, i Translation from: Referativnyy Zhurnal, Mekhanika, 1957, Nr I], p 5! (USSR) AUTHOR: Ginzburg, 1. P. TITLE: The "Water Hammer" in Pipes Made of Elastic-Viscous Materials. (Gidravlic heskiy udar v trubakh iz uprugo-vvA;,.kogo mate riala). PERIODICAL: Vestn. Leningr. un-ta. , 1956, N~ 13, Y9--08 ABSTRACT: The A. establishes the equations of the water hammer in a thin-walled pipe having a varying diameter along its length and consisting of an elastic-viscous or plastic material. Discarding the convective terms and assuming a linear frictional function, these equations are reduced to a single differential equation of the fourth or third order. A general solution for this equation is offered for the case of a cylindrical pipe, obtained by means of a Laplace transformation. T'J'Jiography: 5 references N. A. Kartvelishvili Card I/I AKSWOV, A.P.; GINZBURG, prof., doktor fiziko-matemat.nauk, nauchnyy rukoyoAiik". (Determining the surface temperature and surface friction of cones and a certain class of axisymmatrical bodies of revolution moving with high supersonic speeds; dissertation presented for the degree of Candidate of Physicomathematical Sciences) Opredelenie tempera- tury na poverkhnosti i poverkhnostnogo treniia konusov i nekotorogo klasBa oaasimmetrichnykh tel vrashchaniia, dvizhushchikhoia s bollehimi everkhsvukovymi skoroatiami; avtoreferat diesertateii no soiskanis uchenoi stepeni kandidato fisiko-matematiohaskikh nauk. laningrad, 1957. 7 P. (MIRA 120) (Aerodynamics, Supersonic) (Friction) SOV/124 -58-8-8424 Translation from! Referativnyy zhurnal, Mekhanika, 1958, Nr 8, p IZ (USSR) AuTHOR: Ginzburg, 11. P. T IT L. E: Basic Equations for the Dynamics of the Control of Water Turbines (.Osnovnyye uravneniya dinamiki tegulirovariiya gidroturbin) PERIODICAL.: Uch. zap, 1,GU, 1957, Nr 217, pp 144-184 ABSTRACT: The article gives a detailed account of the derivation of an equation for the process of controlling a water turbine with the aid of a hydraulic regulator. Equations are given for the turbine con- trolled, the sensor element, the servomotors, the gate valve, and the penstocks. The equations evol,,ed are compared with those appearing in the fundamental work on turbine control by A. Stodola The present equations, however, are not investigated. M. A. Ayzerman Card 1/1 10(0) PHABE I BOOK EXPLOITATION SOV/2053 Giazburg, Isaak PavlovIch Prikladnaya, Sidrogazodinamiks (Applied Hydro- and Gas Dynamics) /Laniagrad/ Itd-vo LeninSr. univ., 1958. 337 P. Errata slip inserted. 4,ODO copies printed. Sponsoring Agency; Leningrad. Universitet imeni A. A. 7.hdduova. Redak- tsionnoizdatellskiy movet. Ed.: Ye. V. Shchweleve.; Tech. Ed.: S. D. Vodolagina. PURPOSE: This textbook is for students of physics-mathematics and mathe- matics and meabanics departments at universities and other institutions of higher learning. It may also be use-ALI to engineers and scientific personnel conerned with problem of design and research on engines, gas exhaust, pneumatic installations, etc. Card 1/.U Applied Hydro- and Gas Dynamics SOV/2053 COTERAGE: This textbook on applied hydro- and gas dynamics is based on a series of lectures on mathematical mechanics OLven by the author at the Leningrad State UniYersity. 7he book develops the basic equations of hy- draulics and the theory of similitude and dimensional analysis. It treats uniform and unsteady motions of fluids and gases in straight and curved pipes of uniform and varying cross section, the discharge of fluids and gases from contalmrs, the time required to fill and empty vesselop and the resations of flowing liquids aud gases on rigid boundaries due to mo- mentum changes. Examples of the application of these methods to part- icular engineering problems are presented. Problems of airfoil and cas- cade theory are not discussed since they are fally treated in other books, such as Profissor G. N. Abramovich's Prikladnaya Gazodinamika (Applied Gas DYMNJW),, etc. In view of Professor K. P. Stanyakovich's detailed monograph,Herustanovivsheyesya dvizheniye sploshnoy oredy (Unsteady Notion of a Continuous Medium), the unsteady motion of gases is considered only in connection with the emptying of vessels. Similar3j, problems of un- steady motion of a fluid in rivers and channels are not considered since they can be found in the article by Ac,-demician B. A. Khristianovich Card 2/11 Applied Hydro- and Gas Dynamics SOV/2053 OUnsteady Motion in Channels and Rivers", in the collection Nekotoryye no- vyye voprony mekhaniki sploohnoy aredy (Some New Problems in the Mechanics of a Continuaus Medium) and in V. A. Arkhangel'skiy's monograph Raschety neustanovivahegoeya dvizheniye v otkrytkh vodotokakh (Calculation of an Unsteady Motion in Open Water Currents). There are 69 references., 65 of vhich are Soviet., and 4 translations from German, TAXZ OF CONTMS: Preface 3 Ch. I. Basic Equation of Hydraulics 1. Hydrodynamic quantities and their average values. Basic concepts and definitions 5 2. System of equations of motion of a fluid 9 3. Internal energy,, specific heat., viscosity, and beat conductivity of fluidCand gases 18 Card 3/11 Applied Hydro- and Gas Dynamics SOV/2053 4. Equations for mean local hydrodynamic quantities 25 5. Hydraulic foraulation of the problems and equations of hydraulics 29 6. System of equations of the hydraulics of an incompressible fluid. Bernoulli I a equation 42 7. Examples of the application of Bernoulli's equation to an incom- pressible fluid 44 Bibliography Ch. II. Basic Theories of Similitude and Dimensional Analysis 1. Determination of a W litude 48 2. Basic laws of mechanical similitude 49 3. On approxinate similitude 54 4. Relationship between similitude and dimensions. Jr- theorem 55 5. Exanples for application of the-M - theorem 60 Bibliography 64 Ch. III. Uniform Motion of a Fluid Through Pipes and Channels Card 4/11 Applied Hydro- and Gas Dynamics SOV/2053 1. General relationships for the uniform motion of a fluid in a pipe 65 2. Imminar motion of fluid in a circular pipe 67 3. Limits of applicability of the laws of laminar motion of a fluld. Phenomena occurring in the initial section 69 4. Transition from Unine, to turbulent flow. Critical Reynolds number. Phenomenon of intermittent turbulence 71 5. Results of the ex1mrimeatal investigation of the turbulent motion of fluid in smooth pipes 73 6. Relationship between the friction law and the law of velocity distribution across the amse section of a pipe 77 7. Basic aspects of the samiampirical $heory of turbulence ap- plied to the motion of a fluid through a pipe 81 8. Turbulent notion of fluid in rougb pipes 89 9. On the turbulent motion of a fluid in non-circular pipes 95 BibUography 96 Card 5/ 11 Applied Hydro- and Gas Dynamics Ch. 17. Unsteady Notlon of a Fluid in Pipes SOV/2053 1. Equations of motion of a fluid inpipes 97 2. Equation of state. Internal energy and entropy of the fluid 98 3- Equation determining ve-riation in area of a pipe cross section as a function of pressure 104 4. Boundary and initial conditions 108 5. Solution of the problem of unsteady motion of a fluid in a pipeline without consideration of compressibility 113 6. The work of N. Ye. Zhukovskiy on hydraulic shook in water pipes 117 7. Hydraulic shook in pipes of variable cross section 121 8. Problems of regulation in the presence of hydraulic shook 133 Bl~liography Ch.~.V. Motion. of.,..Gases Jn,,,Fipee 139 I. Equations of motion 140 2. Equations of the steady motion of a gas. Concept of critical speed 142 3. Motion of a gas in pipes of variable cross section 146 Card 6/11 Applied Hydro- and Ou Dynamics SOV/2053 4. Adiabatic motion of a gas In a pipe of variable cross section. The Laval nozzle 147 5- Notion of a gas in a heat-insulated pipe in the absence of an Internal heat source 152 6. Jbtion of a gas in a pipe of constant cross section in the pres- Me of a heat source 156 7. Isotherml wtion of a gas in a pipe 165 8. lamina motion of a gas in flat and circular pipes I& Bibliography 177 Ch YL.. . Loeal-Resistmaps,. Notica of a Fluid and a Gas in Curve& Pipeq. 1. Motion of a fluid in a pipe with a sudden change in cross section 178 2. Motion of a gas in a pipe with a sudden change in cross sea- tion. Shook VaTes 186 Urd 7/11 Applied Hydro- and Gas Dynamics SOV/2053 3- Notion of a fluid in diverging and converging pipes 194 4. Notion of a fluid in nonstraight pipes and channels. Curved -pipes 199 5. Basic conclusions from the results of experimental investiga- tions for determining the local-drag coefficients for branch- ed pipe linesp lattices, nets, ate. 205 Bibliography 214 Ch. VII. Stea4y DiaahwV of fluids and Games from Vessels. Spill- W". 1. Discharge of fluid frm -11 and large openings P-15 2. Discharge from nozzles 218 3- Theoretical methods for determining the coefficients of jet contraction 219 Spillways. Determination of the discharge of fluid through a spillway. Spillway with a wide sill 225 5. Adiabatic discharge of a gas from a vessel through a -11 opening. Analogy with a spillway having a wide sill 233 Card 8/11 Applied Hydro- and Gas Dynamics SOV/2053 6. Diochargecfa gas from a vessel through a long heat-insulated pipe 236 7. Discharge of a gas from a vessel through a long pipe for the case of an isothermal process of gas flow in the pipe 242 8. Discharge of a gaz from a vessel through local resistances 245 9. Discharge of a gas from a vessel through a long pipe and local resistances 254 10. Discharge of a gas from a vessel through a long pipe in the case of laminar flow conditions 257 Bibliography 263 Ch. VIII. Determining the Time Required for Filling and Emptying Vessels of Fluid or Gas 1. Determining time required to empty fluid from a vessel under the assumption of a quasistationary outfl(nr process 264 2. Solution of the problem of determining time required for Card 9/11 Applied Hydro- and Gas Dynamics SOV/2053 equalizing the water levels in two lock ch=bers 266 3. Approximate solution of the problem of emptying a vessel without the assumption of a quasistationary outflow process 267 4. Solution of the problem of determining the time for emptying a vessel of gas flowing through local resistances or a long pipe line and assum- ing the process of outflow to be quasistationary 270 5. Exact solution of the problem of emptying a cylindrical vessel of gas flowing through a small opening in the bottom. Reflection of a shock wave from. the v&L' with the opening Z74 6. Determining the time for filling a vessel with gas 29k 7. Solution of the problem of emptying a variable-volume vessel of gas in the presence of internal fuel combustion 296 8. Determining pressure as a function of time in a chamber where the com- bustion of solid fuel takes place 300 9. Solution of the problem of simultaneous filling and emptying of a vessel of gas 305 10. Examples of engineering applications of the above-mentioned problems 309 Card 10/U Applied Hydro- and (ka Dynamics SM12053 Bibliography 321 Ch. IX. Laws of Momentum and Moment of Momentum and Their Application to the Solution of the Problem of Interaction~Betveen a Flov and Rigid Boundaries 1. Pressure of liquid and gaseous jets on stationary and moving obstacles. The Pelton vhebl 322 2. Determination of the forces and moments with vhich the moving fluid (gas) sets upon the vessels conducting them 329 Bibliography 334 AVAILAME: Library of Congress (QA 93.1 . G49) IS/bg 7/14/59 Card 3-1/1-1 KOVAMV, Maksim Antonovich; BHWVA, Aleksandra Vaoillyevna; KAWVICH. Hatal'ya Hikiuiylavua; LANDW, Vera Oannadiyevna; GIIMURG, I&P#9 prof#o rod.; BUSORGINA, N.I., red.; ZMXOVA, To.G., telchn.rod. [Hnnual for laboratory work on aerognedynamical Rukovodstvo k laboratornym rabotam po aerogazodinamike. Pod red. I.P. Glazburga. Leningrad, Izd-vo Leuingr.univ., 1959. 175 P. (MIRA 13:1) A (Aarohydrodynamics-lbindbooh, manuals, etc.) MSE I BOOK EXPLOITATIOR sOv/5290 Soveshchaniye po prikladnoy gazovoy dinamike. Alma-Ata, 1956 Trudy Soveshchaniya po prikladnoy gazovoy dinamike, g. Alma-Ata, 23-26 oktyabrya 1956 g. (Transactions of the Conference on Applied Gas Dynamics., Held in Alma-Ata, 23-26 October 1956) Alma-Ata, Izd-vo AN Kazakhskoy SSR, 1959, 233 p. Erratft slip inserted. 900 copies printed. Sponsoring Agency: Akademiya nauk Kazakhskoy SSR. Kazakhskiy gosudarstvennyy universitet imeni S.M. Kirova, Editorial Board- Resp. Ed.- L,A, Vulis; V.P. Kashkarov; T,P. Leontlyeva and B.P. Ustimenko. Ed.: V.V. Aleksandriyskiy. Tech. Ed.: Z.P. Rorokina. PURPOSE: This book is intended for personnel of scientific research institutes and industrial engineers in the field of applied fluid mechanics, and may be of interest to students of advanced courses in the field. Card 1/9 Transactions of the Conference (Cont.) SOV15290 COVERAGE: The book consists of the transcriptions Of 31 papers read at the conference on goo dynamics which was convened under the initiative of the Kazakbakiy gosudarstvennyy universitet imni S.M. Kirova (Kazakh State Univer- sity imeni S.M. Kirov) and the Institut energetilti Akademii nauk Kazakhokoy SSR Institute of Power Engineering of the Academy of Sciences Kazakhskaya SSR) and held October 23-26, 1956. Three branches of applied gas dynamics were discussed, namely: jet flow of liquids and gases, aerodynamics of furnace processes, and the outflow of liquids. The practical significance of the "Transactiond'of the conference consists in the adaptation of theory to methods of technical computation and measuring methods related to industrial furnaces and other industrial processes in which aerodynamic phenomena play a predominant role. Eight papers read at the Conference are not included in this collection for various reasons. The authors of the missing papers are: L.D. L'vov (Thermal and Aerodynamic Characteristics of Pulverized Coal Flame Burners) and A.A. Goleyevskiy (Outlines and Physical Models of the Jet Motion Mechanics of Fluids), N.I. Akatnov, Ye. P. Bogdanov, S.V. Bukhman, T.K. Mironenko, A.B. Reznyakov, and G.V. Yakubov. L.G. Loytsyanskiy is mentioned as being in charge of a department of the Kazakh State University, and I.D. Malyukov, Candidate of Physical and Mathematical Sciences, Docent, as a member of the same university. 'Ieferences are found at the end of most articles. Card 2/9 ,rrannactions o-' the Confeirnee (cont. Sov/529n TABLE OF C01IM473: From the Editors Session of Octolxr (23) 1)56 Abramovich, G.11. [Doctor of Technical Sciencer,; Professor; TsW4 imeni Baranova 10entral Scientific Research Instititt.c, of Aircraft Engines imeni P.I. Baranov); Moskovskiy aviatsionnyy institut imeni Ordzhonikidze, 14oskva (Moskow Aviation Institute imeni Ordzhonikidze, Moscow). Turbulent Jets in a Flow of Liquid Ginzburg, I,P. (Doctor of Physical and Mathematical Sciences; lsr*ofessor; Gosudarstvennyy universitet imeni Zhdanova, Leningrad (State University imeni Zbdanov, Leningrad]. On the Outflow of of Gases From Containers Through Pipes in the Presence of Friction and Local Resistances 17 Card 3/9 Transactions of the Conference (cont.) SOV/5290 Vulis) L.A. [Doctor of Technical Sciences; Professor; Kazakhskiy gosudarstviznnyy universitet imeni KirovEL; Institut energetiki AN KazSSR, Alma-Ata) (Kazakh State University imeni Kirorv; Institute of Power Engineering Academy of Sciences Kazakh SSR, Alm Ata)]. Basic Results and Further Problems of Investigating Jet Motion of Liquids and Gases 29 Isatayev, S.I. On the Turbulent Wake Behind a Poorly Streamlined Body 59 Contents of the Discu5sion in Brief Session of October 24, 1956 (Morning) )111 Antonova, G.S. Inveotigating Turbulence Cbaracteriatics of a Free Ponisothermic Jet and an Open Flame 45 Fashl,arov, V.P. (Candidate of Phynical and Mathematical Sciencerfl. r)zl Parallel and Cortiary Motion of Two Uniform Flovs of Cornlressible Gas 55 Card Val Transactiorin of the Conference (Cont.) Lcontlyeva, T,P, (Candidate of Technical Sciences]. ':-,pansion of Axially Symmetrical Jets in Parallel and Contrary Flows 6-, Bukhman, S.V. Regularity of Motion and Combustion of Coal Particles 69 Nazarchuk, M.M.., and N.I. Pollskiy. On the Crisis in the Viscous Flow of Gas In a Plane Parallel Channel 69 Contents of the Discussion in Brief 75 Session of October 24, 1956 (Evening) Terekhina, N.N. Expansion of an Axially Symmetrical Jet of Gas in a Medium of Different Density 77 Chebyshev, P.V. [Vsesoyuzn,,y elektrotekhnicheskiy institut (All-Union Electrotechnical Institute)). Electrothermoanemometers and Their Use in Investigating Noni6othermic Gas Flows 85 Card 5b Tremsactions of the Conference (Cont.) SOV/5290 Trofimnko, A,T. Investigating a Semirestricted Turbulent Jet Akatnov, Nj. Survey of the Works of the Departwnt of Hydronero- dynamics of the Leningrad Polytechnical Tnstitute imeni Kalinin on the Jet Theory 107 Shopelev, S.F., and S. Tsoy, Plane Jet in a Cross Section of an Air Conduit 108 Bespalova, V,G. Use of Hydrointegratora F3r Solving Jet Prcblems 115 Contents of the Discussion in Brief 122 Session of October 25, 1956 (Morning) Katanellson, B,D, [Candidate of Technical Sciences; Docent; Tsentral-Inyy kotloturbinnyy institut imeni Polzunova, Leningrad (Central Turbine and Boiler Institute imeni Polzunov, Leningrad)]. Some Problems of the Aerodynanics of Furnace Cyclone Chambers and of the Combustion of Coal Powder Pulverized Coal 123 Card 619 ,-Iransactior.-. o ' the Conference (Cont,) SOV/5290 1.'stimnkoj, B.P, Candidate of Technical :,cienceri) Ael-Odynamics of an Involute Jet and of a CYclone Chamlx~r 134 Volkov., Ye. V, Sow Aerodynamic Problems of a Two-Phase Flow ir. a Cyclone Furnace 142 Tonkonogiy, A.V., and I.P. Basina. On the Problem of the Working Process in a Cyclone Chamber 152 Yakubov) G.V. Generalizing Aerodynamic Laws of Cyclone Chambers 1~)'q Contents of the Discussion in Brief 158 Session of October 25, 1056 (Evening) Reznyakov, A.B. (Doctor of Technical Sciences; Institut energetiki (Institute of Power Engineering)], Uniflow Flaw of Pulverized Coal 16o Teleginj, A.S. Regularities of Gas Flame Burning 16o Card 7/9 Transactions of the Conference (cont.) SOV15290 Yerchin, Sh. A. Aorodynamica of a Turbulent Gaa Flame.. 16C Kokarev, N.I. [Candidate of Technical Sciences; Urallskiy politekhnicheskiy institut Ineni Kirova, Sverdlovsk (Ural Polytechnical Institute imeni Kirov) Sverdlovsk)]. Industrial Testing of New Gas Heads of Open Hearth Furnaces 178 Bogdanov, Ye, P. On the Thermal Regime of the Gasification Process l86 Contents of the Dincussion in Brief Final Session, October 205, 1956 180 Zhulayev, P. Zh. [Candidate of Technical Sciences; Docent]. Survey of Work on Hydrodynamics Done by the Institut Energetiki ,I.N KazSSR (institute of Power Engineering of the Academy of Sciences Kazakhsb-aya SSR) 187 fiomanen'lco, S,V. Ooccased). Rnzic Problems of Flow Thermodynamics ir Real Baund,3r.-., Conditions 197 Card S/9 Transactior--. o' the Conference (Cont.) Vulicy L.A. On the Circular Motion of a Vincoun Clio Mironenko, T,K. Effect of the Local Mitribution of Ti,qy 2jr in a High Velocity Flow of Gas Mfnhitsp A.G, Flow of Boiling and Hot Water ThrouC~h Conical !'ou.1cs 1-15 Radchenko, G.A., anl P,V, Beloborodov. Concentration Fl,cldr. of i(ighly nisrerned A~roaola In Air ConAnita 2.77 Contents of the Dianuasion in Brief j.x1 sions of tbn Conference WATUME: Library of Congress Card 9/9 X/rn/nas 7-29-1' )1 P" x 3OCK LuwrTxrm" wv/~"30 254p. M.I,.Yy. -r.--kl, lip t-m-4. L-C A. A. L~- FW.F. U.- 1. 9. ILI -d I- r., .f a- .4 -- L. -1-4 31 36 12, -7r 57 9r If bl-i'l 2%-_4 3_~ :,!6 ~f %t. C-~'. r up., I., C~t, ML it. C K~Moslblttf M -&P Aff,-A-Alo 66 17. &-.1 M-4 ITO 7%-U 19. 4ftt_A_A.. WT!- r - ZU.2 -0. f fte~b_ C- q--, 17? ar:- :r .2. :~-,. tf U--t- tb. a;z.m 233 U-pk~ ~,b- J- th. Q~wAtty f t-. tL-: GMBURG, I.P. (Possible methods for solving boundary layer problems in the case of dissociation and diffu8ion; Conference on Heat and Mass Transfer, Minsk, June 5-10p 19611 0 vozmozhriykh metodakh reshe- nlia zadach pogranicbnogo sloia pri nalichii dissotsiatsii i dif- fuzii; soveshchanie po teplo-i massoobmenu, g. Minak, 5-10 Aunia 1961 g. Minsk, 1961. 35 p. (MIRA 15:2) (Boundary layer) (Dissociation) (Diffusion) GINSBURG, 1. P. "On Possible Solution Methods of Problems of a Boundary Layer at Dissociation and Diffusion." Report submitted for the Conference on Heat and Mass Transfer, Minsk, BSSR, June 1961. amemima.- 1. P.. GALANOVAp S. S. , and DWNTYEV, V. G. "Solution of Laminar Boundary Layer Problems With Regard of Radiation and Absorption of a MediUm." Report submitted for the Conference on Heat and Mass Transfer, Minsk, BSSR, June 1961. 20762 SIOA11611000100110041010 LUTHORS Ginzburg, I.P. TITLE: Turbulent boundaa7 layer in a compressible fluid (gas mixture) PERIODICALt Leningrad. Universitet. Vests1k. Seriya matematiki, mekhaniki i astro3wall, no-It 1961P T5-88 TRXTt Starting from the semiempirical theory of turbulenue the author elves an approximate solution of the problem of the determination of skin friction and heat of a plate being in a compressible fluid during a turbulent motion. Dissociation and diffusion are bonsidered, the Prandtl number maj be an arbitrary constant. At first the author establishes the stationary boundary 1sVer equations under consideration of the diffusion and the forces due to inertia. For the determination of the components of the friction tensor and the diffusion and heat vectors the author uses the results of the sea$- empirical theory of turbulence, where the mixing ways in all oases are equated. It is assumed that there exists a laminar lower stratum, where at the boundary of it the derivatives of the velocity, of the heat content and the concentration have jumpe, while the velocity, the heat content and the concentration themselves, as well as the skin friction, Card 113 20762 8104 61/000/001/004/010 Turbulent boundary lsyer... cillYC222 the diffusion and, the beat flow remain continuous. A mmber of further simplifications is made, e.g. it is put T . a h3+b h 2+0 h+d~ (3-3) where T -- Umperature, M - Mi -- molecular weight of the i-th component, A -- relative mass concentration, h h h ? 1 151, 1 -- specific entalpy of the i-th componentl the gas is assumed to be thermodynamically ideal; the friction stress is arranged as a quadratic polynomial in where y -- coordinatelto the plate, E-- thickness of the boundary 1&yer. The equations can be integrated under these and further assumptions., For the velocity distribution in the laminar lower stratum the author obtains v 1+n V +U v2 (8-3) x x x PW where Z is the friction stress at the wall, while pw and n are Card 2/1 20762 S/043J61/000/001/004/010 Turbulent boundary layer... C11I/C222 connected by the arrangement b+dl n (7-3) i~+_dj ) ' where coefficient of the physical tebacity, h -- the h-value at the wall. The author determinest 1. The dependence ofwthe full heat conteut of the velocity. 2. Velocity profile- 3. Thickness of the laxinar lower stratum and the velocity at its boundary- 4. The connection between ~ and S -thickness of the boundary layer- 5. Law of friction. 6.temperature of the surface of the plate- 7. The appearing constants. The author mentions L.Ye.Kallkhman. There are 2 figures, 1 Soviet-bloc and 2 non-Soiiiat-bloc references. The reference to the Raglish-language publication reads as followsi M.Leghthill. J. fluid mech., 2, no.1,1957. Card 3/3 23154 S/024/61/000/003/002/012 0 E140/E463 AUTHORS: Babushkin, S ~). and Ginzburg, I.P. Meningrad) TITLE: On the theory of nonlinear combined and autoromous control systems PERIODICALi Izvestiya Akademii nauk SSSR, Otdeleniye tekhnicheskikh nauk, Energetika i avtomatika, 1961, NO.3, PP.14-30 TEXT; The article attempts to determine the nature of a computer (analogue) for an automatic control system in which k controllers regulate that many system coordinates, such that absolute invariance of the regulated parameters and their autonomy with respect to the other coordinates of the system be obtained. Th system considered in all generality is shown in Fig.1, where A is the object, 8 the computer, the small blocks labelled is .... v , k are the regulators. Furth r yo ( V ~ 1, ..,, k) are the coordinates of the object in k-spac:, xj-)M (J 1 itn)p) describe the motion of the regulators, x %, (VI , " n'O V a ..69 k) is the action applied by the V -th regulator to the object, gq(t) is the input programme to the computer, Ov - Y.0 - g.O(t) are error signals (physically Card 1/7 23154 S/024/61/000/003/002/012 On the theory of nonlinear E140/E463 measured) ~L V M (t ) &j p I V - 1, ..., k) are exle5nal perturbations acting on t~e* ob ect and regul tors, and xi V are the computed control signals. Finally, I v are the functions generated by the computer. Such a system is described by a system of differential equations consisting of three groups of equations: equations describing the motion of the controlled object and the controllers, equations describing the motion of the computer, and k equations describing the errors. It is assumed that the equations of the object are fixed while the equations of the regulators are only slightly varying. The physical measurements and their conversion to computer input signals are assumed inertialess. The object and regulator functions and their partial derivative an well as the computer functions and partial derivative are assumed continuous and bounded over the entire range of possible variation. The computer has k equations for solving the k input signals to the regulators. In these equations there are initially undetermined equations describing as yet unknown corrective networks. The problem posed by the paper can now be stated more precisely. It is required to determine the conditions placed on the computer functions Card 2/7 On the theory of nonlinear ... such that Y gV W S/024/61/000/003/002/012 E140/E463 N = 1, 2, ..., k) (1.2) i.e. that the motion of the object identically correspond to the input programme, as well as the conditions on the equations of the individual regulators and the overall automatic control system, in order that the motion defined by this solution be stable. Such motion is termed: programme motion. Eq.(1.2) permits the system of differential equations of the general system to be simplified by elimination of the static error equations. The second section of the article is concerned with the derivation of the simplified equations. This simplification depends on the fact that for an approximately invariant system, the error terms in the object and regulator equations are negligible (which is not true for the computer equations which depend precisely on the error values). Then a subset of the equations simplify to an autonomous system of N differential equations in N variables, which can therefore be integrated'independently of the remaining k equations of the system. The problem of determining the Card 3/7 23154 S/024/61/000/003/002/012 On the theory of nonlinear 9140/E463 computer function in solved by first substituting the functions of time found for the simplified object and regulator equations in the general expression for the as yet unknown computer functions. By the formulation itself of the problem, the steady state values of the errors are arbitrarily small. Then the functions OV can be expanded close to the plane in which the errors and their derivative vanish in a Taylor series in variations of the error from this plane. This implies that absolu e invariance of the system will occur only when the functions C; vanish identically and the partial derivatives with respect to the errors aye bounded with substitution in them of the functions of time ;ZjJ V)I where the bar indicates the solution of the simplified system. Examining further the conditions placed on the functions it is found that one sufficient solution to the problem is equivalent to a control system using perturbation only. No system operating on deviation alone can satisfy the criteria of absolute invariance and autonomy. The author then derives a system of variational equations which constitute the basis for the final stage of the solution. In the final section, the author examines the question of stability of the motion defined by the solution Card 4/7 S/024/61/000/003/002/012 On the theory of nonlinear ... E140/E463 obtained. The stability problem reduces to the study of the stability of the zero solution of an homogeneous system of linear differential equations with variable coefficients. In a particular case the coefficients of the equations become constants. It is this particular case which is examined in detail in the article. The examination is carried out in two stages, firstly for each of the It coordinates independently and then the system as a whole. The stability conditions are expressed in terms of the roots of algebraic equations. It is found that the stability depends not only on the form of control function, but on the parameters of the controlled object and the regulators. Thus conditions can be obtained for the physical realizability of the system. A brief remark on the general case (where the stability coefficients are variable) indicates that the dependence on the system paramoters holds here as well. In conclusion the author mentions various related questions which have not been treated in the article. The possibility of substantially simplifying the form of the differential equations defining the regulation function or even of excluding from these equations a part of the information Card 5/7 23154 S/024/61/000/003/002/012 On the theory of nonlinear ... E140/9463 external to the the 9-th coordinate system; the elimination of mutual couplings between the regulators; the possibility of using self-adjusting corrective networks in the computer and the inclusion of nonlinear equations in the latter. There are 3 figures and 16 references: 12 Soviet-bloc and 4 non-Soviet-bloc. The four references to English language publications read as follows: Moore, I.R. Proc.IRE, 1951, v-39, Noll, pp.1421-1432; Baksenbom, A.S., Hood, R., NACA, Rep.980, 1950; Aseltine, I.A., Manicini, A.R., Sarture, C.W., Trans. IRE on Automatic Control, PGAC-6, 1958; Margolis, M., Leondes, C.T., IRE Veson Convention Record, 1959, Pt-4, P.104. SUBMITTED; January 23, 1961 Card 6/7 99G 10 il~"oD V~ 21 M43/61/000/004/005/008 D274/D502 AUTHORS: Ginzburg, I.P.t and Focheryzhenkovy G.V. TITLE: Turbulent boundary layer of heat-insulated airfoil or axisymmetric body PERIODICAL: Leningrad. Univer8itet. Vestnik. Seriya matematiki, inekhaniki i astronomiit no. 4j 1961, 115 - 121 TEXT: The problem of gas flow in a turbulent boundary layer is solved by assuming Pr = 1. Velocity profile: It is assumed that the friction stress in the boundary layer can be expressed by wfLl _ (Y)lj+ w((L)_(;L)2 (1.1) where Tw is the shear stress at the wall, the thickness of the boundary layer and y the distance from the ivall; W L ft. T dx1 Card 1/8 w 2~)02'j S/043/61/000/004/L)05/UO8 Turbulent boundary layer of ... D274/D302 the gas is ideal.; equation T R h + d U-3) holds. Hence c 11 + d 11w +cd 1 w = - 1 (1-5) Pw cl h + d d v2 H + - _ A x w c1 2 where Hw is the heat content of unit mass outside the boundary lay- er. The.equations of semi-empirical turbulence theory are used (in conjunction with Bqs. (1.1) and (1-5)) for obtaining the equation for the velocity profile in the turbulent bound ary layer, viz. + d- C, Pa. kIy7 d Vi. It, + A -2 Card 2/8 2)027 S1 04 X61/00(J/004 /005/UO8 Turbulent boundary layer of D274 D302 The presence of a laminar sublayer is aunumed. There one can appro- Xilflately (let: w y2 X Pw Tw dx 2 The velocity tit the boundary of the laminar sublayer is (1-7) V 1 + T u 2 w ]~ dl) 2 k v* -Vl + W Pw Z + pw dx 2 w (19) where v* u V k k W V* The deriv:Aion is examined of relationship between Tw and By expansion in series (of are sin Jcl/k one obtains from -k~ - k, arcsin arcsin ~j In o.- -F k 2 Ub Card 3/8 . " I I -- - ;190~'7 S/U4Ybl/OOO/uO4/vO5ZO08 Turbulent boundary iayer of ... D274 D302 equation F, kS arcein 1-k U6 ki 1 1 2 = D e U where D e (2.1) Vw k -Vl + we In order to find the friction resistance of an airfoil, a second equation between 6 and Tw is required. This can be obtained frow the iaw of conservation of momentum. For using itp one has to xnow the thickness 8** of iost momentum and ihe thickness V of dispia- cement. If, in Their computationg ihe velocity prolile in the boun- dary layer is assumed to be that of a platep one obtains the appro- priate expressiona -L -!L~ (I - 2- ) d PO Pa (2.2) where + Card 4Z8 PQ B/043/61/000/004/005/008 Turbulent boundary layer of ... D274/D302 and 6 + U2 + (2-3) 6** -Vj___~ =u2 _r ... If the influence of the longitudinal pressure gradient is taken in- to account, then C I ~- pv uh k (w) P- 1) L k(,.) --e' (2.6) k2 v. V PO U where HW - Ht. (H. ~+' A Determination of friction lawt In order to find the friction law, i.e. the dependence of ~ on x, the equation 1 d ( rF_ Pou 2s + Pou lu TW (3.1) Card 5/8 rE Nx- dx 2' 027 S/043 61/000/004/005/008 Turbulent boundary layer of D274 D302 is used which expresses the momentum law; a 0 for an airfoil and 1 for an axioymmetric body. One obtains "'d u d in r') - Vr iT _i I Pw -CI (3.2) x V~ where I ft F* P. P- This equation is solved by the method of suc cessive approximation. Setting D k' 2 1 f k arcein U = (X)V f2(X)P k J one obtains ln Po R ln f,(x) + gf2(x), (3-3) Poo For the determin ation of Z = po/pm R one obtains Card 6/8 29027 S/043/61/000/004/005/008 Turbulent boundary layer of ... D274/D302 I dZ Ut 60 a din r' 0-4) z d A- - X_ U_' + 7 __7x_ n, where 2-fn, -If 2e-R, tv~ 1:2 (X) 2 P. if 6*/b.. is considered as a known function of x, then Eq. (3.4) is a linear differential equation whose solution is 7, e- I F. (X) dx IC+ F, (x) eff',(xldx dxl. (3-5) In the case of a plate O)p one obtains for the friction coef- ficient Cf - 2 B"-' Z, (3.6) 2kWle k, nW U, Y4 (D 2. Nt) Card 7/8 2 027 00/61/000/004/005/008 4 Turbulent boundary layer of ... D274/D302 If Fo/pw = ho/Hh , then w (3-7) (amin i Cf = 20'e (D*I) (I -U,)i.. There are 3 Soviet-bloc referencee. Card 8/8 GINZBURG, I.P.; KOCHERYZHM(YV,, G.V. Turbulent boundary layer of a thermally insulated v14 or adayamtrical body, VentsIM 16 no.19:115-121 161. (KIRA 14:10) (Aerodynamico) ad. UrdyaMts 0.- boun 14 6 of- a turbulent A bodi, in Nra ! 0 paper 40: ressim.: 8..A:. 'd 4' 1 diat re on, and, 10 m1w R!ublayer. 3 2 FM INGO 4 ~.I t w :i- oil fri oid pros- MIN y vith~ a radius bad liotiturcTo 700. Ivaid ig 1,6i~ h ill Wl-.Liii I Nil ~4z LXKOVt A.V., akadmik, red.; SMOLISKIY, B.M., doktor tekhn. nauk, prof., red.; GINZBURG,,;,p., doktor fiz.-matem. nauk, prof., red.; ZAMDSXTY, doktor takhn. nauk, red.; KONAKOV, PA., doktor tekhn. nauk, prof., red.; KOSTERIN, S.I.,doktor tekhn. nauk, prof., red.; SHULIMAN, Z.P., inzh., otv. za vypusk; KORIKOVSKIY, I.K., red.; JARIONOV, G.Ye., tekhn. red. tHeat and mmaD transfer) Teplo- i massoperenos. Moskva, Gos- energoizdat. Vol.3.[General problems of heat transfer) Obahchie voprony teploobmena. 1963. 686 p. (MIRA 16:6) 1. Akademiya nauk Belorusakoy SSR (for Lykov). (Heat-Transmission) (Mass transfer) I GINZEURG, K~A;HIRYZHEKKQV, G.V, Turbulent boundary layer rf a nonthermlly inaulated wing or axisymu-frl-v body in a compreasible fluid. Yast,L&U 18 no.7t N--98 163. (KMA 16 j4) (Aerotbermodynamics) (Boundary layer) VERESHCHAGINA, L.I.; GINUUM, I.P., prof., rukovoditall raboty Base prossure for solidn of ravoliftion In supertionic gas flow. Vest. UIU 18 no.13WI-143 163. (MIRk 160) (Aarodynarnicn, Supersonic) ACCIZSION IM i 0404M,16 S/0170/64/000/001;/WWOO,74 AUTHOR: Ginsburg, L F, TITLE: The rolationship between heat content and velocity in the boundary layer of flowing gas SOME: Inahenerno-fizicheskiy zhurnal, no. 8, 19(-'+, 64-74 TOPIC TAGS: boundary layori heat transfer, Prandtl number, laninar flow, turbulent flow, Lewis numbor ABSTRACT: An approximate relationship between heat content h and flow velocity v. for arbitrary values of Pr in turbulent as well as in physical flows was established using the boundary layer equations in Crocco variables. On the assumption that Lai = 1 and PtL = const in the boundary layer, general exprossions aro derived for the coefficients R( and S 1/4 ,Card ACUSSION NRt AP1.041AI6 rexp d ip) d tf PFr (0)p 0 dip ROP, 0 - 2 prexp(-~.(1-pr)-de d,? X fm Ip X ~ exp d-p)dtpj~ 0 where vx/Up V and for 0 w 1, R becomeo the recovery facto'r. The vnlues of R(1,9 and S(l,f are thon daterodned for laminar boundary layors- turbulent boundary layer, aseuming a eubla~yer PFA) PrI* ,_~~bulent boundary layere aasuming Van-Driest's three-layer approximationp and 2A Card AFM=M']Mj V404"16 -Anv%mI=t bmmdwy layarr vith - pma AWw1va-hadty of SmIaWk and Vnrobaikm. Fimllyq S and -R-mm eMbeiWed for Pr if I with the 7=ult SO) Pr, + Pr, ) Pr~ r(PrIr(i13) Vr~ WIJ Pf. rift, + 1/3) R(J) pr.#e Prql AM where 0 -q0'-PqdIP T .. . 1~ , for Pr = 1 in the presence of flow injection at the wall the values of R and 8 take a modified fom given bV S(II-Sor.) + , - (I -,), Pr. R (1) - R (tf.,) + (I - TI). These results show the effect of Pr (turbulent and laminar) on heat transfer to the walls from the boundary layer and establish a relationship between h and ve Orig., art. hass 66 fomulas and 2 figures. Card 3A ACCWION NRI Ap4o4W6 ASSOCIATIONt Gostidarstvaniq*V univeraitet im A, A, Zdanova g. Lenin grad (Leningrad State University) SUBKTTEDs 22ROV63 ENGLs 00 SUB COIEs NEtTD NO W SOVs 005 MIER 1 000 Card 4/4 GIMBURG, I.P. (Lwdnerad) .111-1:1. OOn the solution of problem of the turbulent boundan, lkyer in a compressible fliid-gaB mixture". report presented at the 2nd All-Union Congrss on Theoretical and Applied Mechani-cs, Hoscow, 29 Jan - 5 Feb 64. ----7-77 o.p 7 7z 151 rq.ort. nubriiltte~l Ibr .,rid All-Unlort Cont' on Heat Mhwk, )1-1:, cA' M!Itl!euutt-,k!:; Mloch?tui-c, lo~ldtwxad ~Illiv. GIHZBURG~ 1.1'. Relation betwoon tho enthalpy and volocity of a gas moving in a boundury layer. Inzh.-fiz. zhur. 'I Z10.8-.64-74 Av, 164. A/ (mlia 1,7-10) 1. Gosudarfl tver-nyy un Lvtiroi tc t im. A. A. , Lo- VAL11,111,1111, ; 6 , I JI.; POLYAKOV, ; YlIS"I"HM', P-i'- Koruqt-an%*"n jvarjovi*~,,h Strakhavich, 1905- ; on his Wth birthday. jn7h.-fjz. zhur. 8 rio.3:409-410 Mr 165. (,'417A 16: 5, 1 )/9Td/ZPF(n)-2AV0(m)AWA(d)/. hmp N4~ 11) AC0968iON N~-. 456i6w UR/0170/65/009/002/0166/0162 632.617A 71 AU Thl 0 4 I oiol.7 Korniv*i 10 v4 TITLE-. The aftect of th-0. turbulent number Prt on the friction imlyheat-kmfe of IL plate !in turbulent gao.fliaw t SOtQRCH, Inzholnorno-fi~ich'askly zhurn4l, v, 9, no.2, 1966g 156-162 TOPIC TAGS: TrIction,00mmelant,' heat transfer, plate, turbulent flow, gas floif ,Prudtl ABSTRACT: Ilie follow! sion was obtained elsewhere (Ginzburg, 1. P. IFZh. .,No. to 1964.) to 4terniI46'the relatl6nihip between the heat content and flow ute in the Ic"a Of nongradiefit flow iM itrbltraiOr and Prv (where Land -ware laminar and turbulent i~ !1. ~ , 4 'flow; respectlyd! )t Card 1/3 0201 L 5~53-66 ACCESSION NR... AP6020947 ---: ivhero X ;Pr a -o (I/Pr dV d1pi Pe 2 Or d4p Pr !xP x e-0 (1a) x 4 V1pr - 1) dp] d alp 'no resent authors use this expreselofi and the basic premises in the oemlempiric theory of tuibulence to ovaluatethe effect 6f,the Pr.V,ntLmber on the friction and heat transfer. coefficient of a plate, 04'. art. Mai 16'numboreed formula. Card 23 L A&O 04 dio&imo Leningrat(Len :,11 1 It i 2 A I ~' 1, !,!.. B 8UB mnat, WAR Aop -1,01, r A ~j: 5,; T i~Wd pj~: 1! Fir, I. )_;I/rWa(pL)jFC8tk)/MA(I)' WN, IS4COUM Mi A119 N16 Trotratlesi SQUI(CE CODX: UR/0170/65/0091004/0444/A-so IF AUTHOR: 0Aurg .4 (09 P.; K!~Oeyqnj(nova, 'M S. OHO: giate Oqyors 'thdanov, Leiningrad (Gosudarstvennyy unive roltet) 71 TITLE: The tuibuleo boundary layer on a plate in an incompressible fluid with blowing of aiostancO! S05m: in verno+.f~iichoskiy zhurnal, v. 9, no. 4, 1965, 444-450 qV, TOOIC TAGSI'~ t d'" laver, -heat trans er, incompressible now, Mrbgl Oti hOun a R*,olds nunibdr AB~TRACT:. tbO We# of blowing on surface friction and heat transfer in the case o fi turbulent! b6uni 14yer h4i been treated previously. To solve the resulting eud the thickness of the ooons4 co#14in siij~olbmtnt4ry ao0umptions were made as to i'iar;Onar~subI4~ror iiWfo the 461ocities at its boundary. The present article consi- deris the effect Of blo*ing on the,parameters of the boundary layer and on friction, on the basis e t*d~layer s~I~emd:o 6 f the semiempirical theory of turbulence. To 'Confirm thNe ihdidit~~W the limiting (boundary) laws proposed previously, and to simplify the ciklculatl~LrW, the present article considers the case of an incompressi- W ifluid. Th6 drtlcl~i 44velopd On approximate numerical solution of the basic equa- UDC:532.517.4 ~Cqrdi/2 'Acc 1~0,A 51 adenc~ of the r44tive friction coefficient on the blowing par ,tiono. The depoi ameter ,is s6oWn in a lioure. iThi - resu~ti catculsted by, the proposed scheme, with a finite r, A ho -to e"riniental results than the results 61 lo W ajOje~r ~~Reix~,,aumbeo reVious worict In tho'll ting i~p. tkoe 'when Re. qproaches infinity, the results jkrt. 4sV25 fomulas, 9 figures and I table 6 n ~de. ii: .01M CODE: M~f SUBM DATE:11 BJan$5/ ORIG REP: 005/ OTH REP: 002 ewd 2/2 tz 612M) T , s , "Chronic VIcerative Gin.-ivitio," Stomatoloptya, liod, 1952 GDMBURG, I.$., doteent, kandidut meditninskilch nauk; NOVIK. 1.0.. doteent. zave- duy.uahchty; GOHGWOV. A.K., professor, direktor. Pathogenic therapy of ulcerative stomatitis. Stomatologlia no.4:10-15 Jl- Ag '53. (MUIA 6:9) 1. I(afedra terapevticheekoy stomtologil Kiyevskogo meditainakogo stomatolo- gichaskogo inntituta (for Novik). 2. Kiyevf;kiy meditainekiy stomutologiohe- skiy institut (for Gorchakov). (Stomatitis) GINZBURG' I.S., bod'dat meditsinakikh neuk Role of vasoular changea in the periodontal tissues in the pathogenesis of parwl~ntosis. Stomatologila, no-3:12-16 Itr-Je 154 C' (HLBA 7 t 6) 1. Is kafsdry terapevticheslooy stomatologii(zav. doteent 1.0. lovik) i kafedry patologicheekoy aziatomil (say. prof. 1.K. Psyss'- Ithovich) kiyovakogo mditminskogo stonatologlehookogo instituta 11r. prof. A.K.Gorobakov) (MIODONTIUX, diseases. Opathogen., periodontal vase. changes) (MIODMIUM. blood supply, Ovase, changes in pathogen, of periodontosis) GIMURG, I.S. Pathogenesis aM therapy of hypartrophic gingivitis. Stomatologlia nn.4:61-64 Jl-itg 155. ( MLRA 8-10) 1. In kafattry torapevticheskoy atomatologil (zav.dotannt I.O.Novik) Kiyevskogo mmditsinskogo atormitologichnakogo inRtituta. (GIRIS-DISUSIS) NOVIK, 1.0., prof.; GINZBURG I S...dotoent (Kiyev) ... !A *Principleo of the nathological anatomy of the oral cavity and teeth* by I.M. Peisakhovich. Reviewed by 1.0. Novik, I.S. Ginzburg. Vrach. dolo no.4:431-433 AP 159. (KIRA 12-7) (STOMATOIA)GY) (PICISAKMVIGH, 1. 14. ) GIMOnG, I.S.; ITASIROT, A.B. Some peculiarities in the pathogenesis and clinical aspects of tuberculous lymphademitis vith aim external and mesenterial looa,. lization. no.2:14-18 7 160. (KMA 13:5) (LTKMTICS--TUBlEtC=SIS) VAYSBIAT, Solomon Haumovich, zeal. deryatall nauki USSR, prof.j GINZBUNG, J,S , red.) MOV, N.M., tokhn. red. (local anesthesia for operations on the face, the jaws, and the teeth]Meatnoe obazbolivaule pri operateftakh na litee, cheliustiakh i zub&kh. Kiev, Goamedizdat USSR, 1962. 468 p. (MIRA 160) (MCiL ANESTHESIA) (FACE-SURGERY) (JAWS--SURGERY) (ANESTHESIA IN DFJTISTRY) GIVZBM, I.S. prof,, jasluzbennyy deyatell naukij KAIPAROV, K.I., aspirant. Phlegman in the newborn and infants during the first year of life, Azmrb. mod. zhur. no.10-3-1 A !62. (MIRA 1615) 1. 14 tafedry II gospitallnoy i detskoy khirurgii pediatriches- kogo takulltata (zav.-Prof, I.S.Ginzburg) Azerbaydzhanskogo go- sudarstvemop meditsinskogo instituts. imeni V.Varimanova (rektor zaslu*hennyy daystell nauki, prof. B A, B~yvazov). (COBECTIVE TISSUES.-DISWM) iMANTS-DISEASES) GINZEURG, I. S.. (Zly") Sme characteriatios of peradentium vascularization and its ollnical oignificance. Problootom. 613&-41 162. (MM 1613) (GUMS-ma SUPPLY) NOVIX, Isaak OBipovicb, prof.; GINZBEMG, I.S., red. [Pariodontosisj pathogenesiBp clinical aspects and treatment) Parodontosl patogenesp klinika i lechenie. 2., Ispr. i dop. izd. Kiev, Zdorovlial 1964. 325 P. (141RA M12)