Separated Flows and Jets - Home - Springer978-3-642-84447-8/1.pdf · of the physics of separated...

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Separated Flows and Jets

Transcript of Separated Flows and Jets - Home - Springer978-3-642-84447-8/1.pdf · of the physics of separated...

Separated Flows and Jets

International Union of Theoretical and Applied Mechanics

v. V. Kozlov, A.V. Dovgal (Eds.)

Separated Flows and Jets IUTAM-Symposium, Novosibirsk, USSR July 9 -13, 1990

Springer-Verlag Berlin Heidelberg New York London Paris Tokyo Hong Kong Barcelona Budapest

Prof. V. V. Kozlov Dr. A. V. Dovgal

Inst. of Theoretical & Applied Mechanics Siberian Branch of the USSR Academy of Sciences Novosibirsk 630090 USSR

ISBN-13: 978-3-642-84449-2 e-ISBN-13: 978-3-642-84447-8 001: 10.1007/978-3-642-84447-8

This work is subject to copyright.AII rights are reserved, whetherthewhole orpart ofthe material is concerned, specifically the rights of translation, reprinting, re-use of illustrations, recitation, broadcasting, reproduction on microfilms orin otherways,and storage in data banksDuplication of this publication or parts thereof is only permitted under the provisions of the German Copy­right Law of September 9, 1965, in its current version and a copyright fee must always be paid. Violations fall under the prosecution act of the German Copyright Law.

© Springer-Verlag, Berlin Heidelberg 1991 Softcover reprint of the hardcover 1st edition 1991

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Scientific Committee

V.G.Dulov, USSR (Chairman)

V.V.Kozlov, USSR (Vice-Chairman)

S.H.Bogdonoff, USA

D.H.Bushnell, USA

F.Durst, FRG

K.Gersten, FRG

Ch.M.Ho, USA

J.L. Van Ingen, NETH

M.Kiya, JAP

E.Krause, FRG

J.C.1eballeur, FRA

Sir James Lighthill, UK (ex officio)

F.T.Smith, UK

S.W. Van Atta, USA

Symposium Sponsors

International Union of Theoretical and Applied Mechanics (IUTAM)

Central Research Institute of Machine-Building, USSR

Siberian Research Institute of Aviation named by S.A.Chaplygin,

USSR

Introduction

Separated flows and jets, being the subjects of individual

branches of aerodynamics, are closely linked in a variety of

applications. They are of paramount importance in various fields

of fluid mechanics including vehicles efficiency, technical

branches bound up with gas/liquid flows, atmospheric effect on

various constructions, etc. The future progress in these fields

is associated, in a large measure, with the extend of knowledge

of the physics of separated flows and jets, achievements in the­

oretical approaches and calculations as well as development of

perfect control techniques.

These aspects were in focus of IUTAM-Symposium which was

held in Novosibirsk, 1990. About 120 presentations and well­

guided general discussions which took place indicated wide in­

terest to the themes of the Meeting. The volume is composed of

the contributions arranged according to their place in the

scientific programme of the Symposium. Thus, the following

main sections may be distinguished, conditionally to some ex­

tent: numerical simulations and theoretical approaches - general

aspects, incompressible turbulent boundary layer separation,

shock waves/turbulent boundary layer interactions, control tech­niques, laminar separation and instability, organized structures

in jets, separated flows and mixing layers. Surely, inspite of great number of contributions the material do not exhaust all

the problems associated with separated and jet flows, but gives

insight into the main research fields. An interested reader will

find here the state of the art, the leading trends and will be

given a chance to avaluate the progress achieved since the pre­

vious IUTAM-Symposium on Boundary Layer Separation, London,19B6.

V.V.Kozlov & A.V.Dovgal

Institute of Theoretical and

Applied Mechanics, Siberian Branch of the USSR Academy of

Sciences, Novosibirsk

Participants

Albazarov B. Sh. USSR Computing Center, Siberian Branch, USSR Academy of Sciences, Krasnoyarsk 660036

Al-Maaitah A.A. Jordan Dept. of Mechanical Engineering, Mu'tah University, P.O.Box 7, Mu'tah, Al-Karak

Althaus W. Germany Aerodynamisches Inst. der RWTH Aachen, Wullnerstrasse zw.5-7, 5100 Aachen

Arnal M. Germany Lehrstuhl fur Stromungsmechanik, Technische Universitat Munchen, Arcisstrasse 21, 8000 Munchen 2

Artamonova M. S. USSR Moscow State University, 119899 Moscow B-234

Bakker P .G. NETH Faculty of Aerospace Engineering, Delft University of Technology, P.O. Box 5058, 2600 GB Delft

Bartsch P. Germany Inst. fur Luft- und Raumfahrt, Technische Universitat Berlin, Marchstrasse 14, 0-1000 Berlin 10

Basin M.A. USSR Krylov Ship-Building Research Institute, Leningrad 196158

Belotserkovsky S.M. USSR Central Aero-Hydrodynamic Institute, Moscow 107005

Bezrukov A.A. USSR Computing Center, Siberian Branch, USSR Academy of Sciences, Krasnoyarsk 660036

Bogdonoff S.M. USA Mechanical and Aerospace Engineering Dept., Gas Dynamics Laboratory, Princeton University, Princeton, NJ 08544

Black D.W. USA Iowa State University, 323 Town Engineering BLdg, Ames, Ia 50010

Bogolepov V.V. USSR Central Aero-Hydrodynamic Institute, Zhukovsky-3, Moscow Region 140160

Boiko A.V. USSR Inst. of Theoretical and Applied Mechanics, Siberian Branch USSR Academy of Sciences, Novosibirsk 630090

VIII

Borisov A.V. USSR

Borovoi V.Ya. USSR

Brodetsky M.D. USSR

Bushnell D.M. USA

Bychkov N.M. USSR

Castro I.P. England

Cherny S.G. USSR

Chernyshenko S.I. USSR

Christov C.I. Bulgaria

Comte P. France

Cui E. China

Dallmann U. Germany

Dikovskaya N.D. USSR

Doerffer P. Poland

Dong Y. China

Inst. of Theoretical and Applied Mechanics, Siberian Branch USSR Academy of Sciences, Novosibirsk 630090

Central Aero-Hydrodynamic Inst., Zhukovsky-3,Moscow Region 140160

Inst. of Theoretical and Applied Mechanics, Siberian Branch USSR Academy of Sciences, Novosibirsk 630090

NASA Langley Research Center, Hampton, Virginia 23665-5225

Inst. of Theoretical and Applied Mechanics, Siberian Branch USSR Academy of Sciences, Novosibirsk 630090

Dept. of Mechanical Engineering, Eniversity of Surrey, CU2 5XH Guilford

Inst. of Theoretical and Applied Mechanics, Siberian Branch USSR Academy of Sciences, Novosibirsk 630090

Inst. of Mechanics, Moscow State University, Moscow 119899

Laboratory of Informatics, Hydro­meteorology Service, Bulgarian Academy of Sciences, Sofia 1184

Inst. de Mecanique de Grenoble B.P.53X-38041, Grenoble Cedex

Beijing Institute of Aero­dynamics, Beijing

Inst. fur Theoretische Stromungs­mechanik DLR, Bunsenstrasse 10, 0-3400, Gottingen

Inst. of Theoretical and Applied Mechanics, Siberian Branch USSR Academy of Sciences, Novosibirsk 630090

Polish Academy of Sciences, IFFM, 80-952, Gdansk

China Aerodynamic Research and Dev­elopment Center, Beijing 100086

IX

Dovgal A.V. USSR Inst. of Theoretical and Applied Mechanics, Siberian Branch USSR Academy of Sciences, Novosibirsk 630090

Efimtsov B.M. USSR Central Aero-Hydrodynamic Institute, Moscow 107005

Epifanov V.M. USSR Bauman Technical University, Moscow 107005

Feng Y. China Beijing University of Aero-nautics and Astronautics, Beij ing 100083

Gimranov E.G. USSR Ufa Aviation Institute, Ufa 450000

Glebov G.A. USSR Kazan Aviation Institute, Kazan 420084

Glotov G.F. USSR Central Aero-Hydrodynamic Institute, Zhukovsky-3, Moscow Region 140160

Gogish L.V. USSR Central Institute of Aviation Motorbuilding, Moscow 111250

Goldshtik M.A. USSR Inst. of Thermophysics, Siberian Branch, USSR Academy of Sciences, Novosibirsk 630090

Gurevitch Yu.G. USSR Central Institute of Aviation Motorbuilding, Moscow 111250

Gushchin V.A. USSR Inst. of Computer Aided Design, USSR Academy of Sciences, Vavilov St.40, Moscow 117959

He Ch. China Aerodynamics Research Society, Beijing

Hipp-Kalthoff C. Germany Inst. A fur Mechanik, Universitat Stuttgart, Pfaffenwaldring 9, 7000 Stuttgart 80

110 C.M. USA Dept. of Aerospace Engineering, University of Southern California, Los Angeles, California, 90089-1191

Horstman C.C. USA NASA Ames Research Center, Moffet Field, California 94035

x

Ilsing T .D.

Huang D.

Hussain F.

Van Ingen J.L.

Iosifov K.

Kachanov Yu.S.

Karavaev E.A.

Karpov A.I.

Kharitonov A.M.

Khlapov N.V.

Khlebnikov V.S.

Kiya M.

Knight D.D.

Konotop T.V.

China

China

USA

Nh"'TH

Bulgaria

USSR

USSR

USSR

USSR

USSR

USSR

Japan

USA

USSR

Beijing University of Aero­nautics and Astronautics, Beij ing 100083

Peking University, Peking

University of Houston, Houston, TX 77204-4792

Faculty of Aerospace Engineering, Delft University of Technology, Kluyverweg 1, 2629 HS Delft

Bulgarian Ship Hydrodynamic Centre, Varna 9003

Inst. of Theoretical and Applied Mechanics, Siberian Branch USSR Academy of Sciences, Novosibirsk 630090

Siberian Research Institute of Aviation, Novosibirsk 630015

Khabarovsk Poly technical Institute, Khabarovsk 680035

Inst. of Theoretical and Applied Mechanics, Siberian Branch USSR Academy of Sciences, Novosibirsk 630090

Central Aero-Hydrodynamic Institute, Moscow 107005

Central Aero-Hydrodynamic Institute, Zhukovsky-3, Moscow Region 140160

Dept. of Mechanical Engineer­ing, Hokkaido University, Sapporo 060

Dept. of Mechanical and Aerospace Engineering, Rutgers University, New Brunswick, NJ 08903

Central Aero-Hydrodynamic Institute, Zhukovsky-3, Moscow Region 140160

Kornienko E.S. USSR

Kornilov V. I . USSR

Korobitsin G.P. USSR

Korolev G.L. USSR

Kozlov A.P. USSR

Kozlov V.V. USSR

Kudrjavtsev V.V. USSR

Kuibin P.A. USSR

Krothapalli A. USA

Kubota H. Japan

Lapygin V.I. USSR

Larichkin V.V. USSR

Le J. China

Leibovich S. USA

Central Research Institute of Machine-Building, Kaliningrad, Moscow Region 141070

Inst. of Theoretical and Applied Mechanics, Siberian Branch USSR Academy of Sciences, Novosibirsk 630090

Inst. of Applied Mathematics and Mechanics, State University of Tomsk, Tomsk 634010

Central Aero-Hydrodynamic Institute, Zhukovsky-3, Moscow Region 140160

Kazan Aviation Institute, Kazan 420084

Inst. of Theoretical and Applied Mechanics, Siberian Branch USSf{ Academy of Sciences, Novosibirsk 630090

Central Research Institute of Machine-Building, Kaliningrad, Moscow Region 141070

Inst. of Thermophysics, Siberian Branch, USSR Academy of Sciences, Novosibirsk 630090

XI

Dept. of Mechanical Engineering, FAMU/FSU College of Engineering, Tallahassee, Fl 32316

Dept. of Aeronautics, Faculty of Engineering, University of Tokyo, Bunkyo-ky, Tokyo 113

Central Research Institute of Machine-Building, Kaliningrad, Moscow Region 141070

Inst. of Theoretical and Applied Mechanics, Siberian Branch USSR Academy of Sciences, Novosibirsk 630080

China Aerodynamic Research and Development Center, Beijing 100086

Upson Hall, Cornell University, Ithaca, NY 14853

XII

Lilienblum V.

Lipatov 1.1.

Lisenkov loG.

Logvinovich G.V.

Lu Zhi Yong

Lunev V.V.

Lushin V.N.

Lysenko V. I .

Maksimov A.I.

Mao Sun

Masuda S.

Meiburg E.

Meier G.E.A.

Michalke A.

Germany

USSR

USSR

USSR

China

USSR

USSR

USSR

USSR

China

Japan

USA

Germany

Germany

Technische Universitat '"Otto von Guericke'", Magdeburg 3010

Central Aero-Hydrodynamic Institute, Zhukovsky-3, Moscow Region 140160

Inst. of Theoretical and Applied Mechanics, Siberian Branch USSR Academy of Sciences, Novosibirsk 630090

Central Aero-Hydrodynamic Institute, Moscow 107005

Beijing University of Aeronautics and Astronautics, Beijing 100083

Central Research Institute of Machine-Building, Kalin ingrad, Moscow Region 141070

Siberian Research Institute of Aviation, Novosibirsk 630015

Inst. of Theoretical and Applied Mechanics, Siberian Branch USSR Academy of Sciences, Novosibirsk 630090

Inst. of Theoretical and Applied Mechanics, Siberian Branch USSR Academy of Sciences, Novosibirsk 630090

Beijing University of Aero­nautics and Astronautics, Be ij ing 100083

Faculty of Science and Technology, Keio University, Yokohama 223

Center of Fluid Mechanics, Division of Applied Mathematics, Brown University, Providence, RI 02912

Inst. fur Experimentelle Stromungsmechanik DLR, 0-3400 Gottingen

Technische Universitat Berlin, Sekr. HFl, Strasse des 17 Juni 135, 1000 Berlin 12

Mikhailov V. I. USSR

Mironov S.G. USSR

Miyake Y. Japan

Panov B.Ph. USSR

Panovko M.Ya. USSR

Pavlyuchenko A.M. USSR

Prudnikov Yu.A. USSR

RoUnnayer A.P. USA

Ruban A. I. USSR

Ryzhov O.S. USSR

Sadovsky V.S. USSR

Safarik P. CZECHOSLOV

Saltanov N.V. USSR

Central Aero-Hydrodynamic Institute, Zhukovsky-3, Moscow Region 140160

Inst. of Theoretical and Applied Mechanics, Siberian Branch USSR Academy of Sciences, Novosibirsk 630090

XIII

Dept. of Mechanical Engineering, Osaka University, Suita, Osaka 565

Leningrad State University, Leningrad 199164

Mechanical Engineering Research Institute, USSR Academy of Sciences, Moscow 101830

Inst. of Theoretical and Applied Mechanics, Siberian Branch USSR Academy of Sciences, Novosibirsk 630090

Siberian Research Institute of Aviation, Novosibirsk 630015

Iowa State University, 326 Town Engineering Bldg., Ames, IA 50010

Central Aero-Hydrodynamic Institute, Zhukovsky-3, Moscow Region 140160

Computing Center, USSR Academy of Sciences, Vavilov St. 40, Moscow 117967

Central Aero-Hydrodynamic Institute, Zhukovsky-3, Moscow Region 140160

Inst. of Thermomechanics, Czechoslovak Academy of Sciences, Dolejskova 5, 18200 Praha 8

lnst. of Hydrodynamics, Ukrainian Academy of Sciences, Kiev 252057

XIV

Schetz J.A.

Schulte-Werning B.

Semenov N.V.

Settles G.S.

Sherbakov V.A.

Shevelkov S.G.

Shilein E.H.

Shkvar E.A.

Shokin Yu. A.

Shtern V.N.

Shumsky G. M .

Simakin I.N.

USA

Germany

USSR

USA

USSR

USSR

USSR

USSR

USSR

USSR

USSR

USSR

Virginia Polytechnic Institute and State University, Blacksburg, Virginia 24061

Inst. fur Theoretische Stromungsmechanik DLR, Bunsenstrasse 10, 0-3400 Gottingen

Inst. of Theoretical and Applied Mechanics, Siberian Branch USSR Academy of Sciences, Novosibirsk 630090

Gas Dynamics Laboratory, Penn. State University, 303 ME Bldg., University Park, PA 16802

lnst. of Theoretical and Applied Mechanics, Siberian Branch USSR Academy of Sciences, Novosibirsk 630080

Inst. of Theoretical and Applied Mechanics, Siberiilll Branch USSR Academy of Sciences, Novosibirsk 630090

Inst. of Theoretical and Applied Mechanics, Siberian Branch USSR Academy of Sciences, Novosibirsk 630090

Inst. of Civil Aviation Engineers, Kiev 252058

Computing Center, Siberian Branch, USSR Academy of Sciences, Krasnoyarsk 660036

Inst. of Thermophysics, Siberiml Branch, USSR Academy of Sciences, Novosibirsk 630080

Siberian Research Institute of Aviation, Novosibirsk 630015

Central Aero-Hydrodynamic Institute, Zhukovsky-3, Moscow Region 140160

Simonov O.A. USSR

Smith F.T. England

Sokolov E.I. USSR

Strobel H. Germany

Stucke P. Germany

Suleimanov Sh. USSR

Sutton E.P. England

Suzuki K. Japan

Sychev Vic.V. USSR

Sychev Vlad. V . USSR

Tararykin 0.1. USSR

Tarasov S.B. USSR

Terentiev E.D. USSR

Dept. of Multiphase Fluid Mechanics, Siberian Branch, USSR Academy of Sciences, Tyumen 625003

Dept. of Mathematics, University College London, Gower Street WC1E 6BT London

xv

Leningrad Mechanical Institute, Leningrad 198005

Institut fur Mechanik, Karl-Marx-Stadt 9010

Inst. of Mechanics, University of Hannover, Appelstrasse 11 3000 Hannover 1

Inst. of Theoretical and Applied Mechanics, Siberian Branch USSR Academy of Sciences, Novosibirsk 630090

Pembroke College, Cambridge CB2 lRF

Dept. of Aeronautics, Faculty of Engineering', University of Tokyo, Bunkyo-ku, Tokyo 113

Central Aero-Hydrodynamic Institute, Zhukovsky-3, Moscow Region 140160

Central Aero-Hydrodynamic Institute, Zhukovsky-3, Moscow Region 140160

Inst. of Theoretical and Applied Mechanics, Siberian Branch USSR Academy of Sciences, Novosibirsk 630090

Kazakh State University, Alma-Ata 480121

Computing Center, USSR Academy of Sciences, Vavilov St.40, Moscow 117967

XVI

Todorov M.D. Bulgaria

Trigub V.N. USSR

Trofimov V.M. USSR

Ugriumov E.A. USSR

Vasilev V.I. USSR

Vedernikov Yu.A. USSR

Vlcek V. CZECHOSLOV

Voitkova, G.V. USSR

Voropaev G.A. USSR

Werle H.C. France

Wu K. China

Yakovlev V.N. USSR

Yavorsky N. 1. USSR

Yurchenko N.F. USSR

Laboratory of Informatics, Hydrometeorology Service, Bulgarian Academy of Sciences, Sofia 1184

Central Aero-Hydrodynamic Institute, Zhukovsky-3, Moscow Reg~on 140160

Inst. of Theoretical and Applied Mechanics, Siberian Branch USSR Academy of Sciences, Novosibirsk 630090

Leningrad State University, Leningrad 199164

Central Institute of Aviation Motorbuilding, Moscow 111250

Inst. of Theoretical and Applied Mechanics, Siberian Branch USSR Academy of Sciences, Novosibirsk 630090

Inst. of Thermomechanics, Czechoslovak Academy of Sciences, Dolejskova 5, 18200 Praha 8

Central Research Institute of Machine-Building, Kaliningrad, Moscow Region 141070

Institute of Hydrodynamics, Ukrainian Academy of Sciences, Kiev 252057

30 avo de Lattre de Tassigny 92360 Meudon la Foret

China Aerodynamic Research and Development Center, Be ij ing 100086

Inst. of Theoretical and Applied Mechanics, Siberian Branch USSR Academy of Sciences, Novosibirsk 630080

Inst. of Thermophysics,Siberian Branch, USSR Academy of Sciences, Novosibirsk 630090

Inst. of Hydrodynamics, Ukrainian Academy of Sciences, Kiev 252057

XVII

Zakharenkov M.N. USSR Central Aero-Hydrodynamic Institute, Zhukovsky-3, Moscow Region 140160

Zametaev V.B. USSR Central Aero-Hydrodynamic Institute, Zhukovsky-3, Moscow Region 140160

Zanin B.Yu. USSR Inst. of Theoretical and Applied Mechanics, Siberian Branch USSR Academy of Sciences, Novosibirsk 630090

Zapryagaev V.I. USSR Inst. of Theoretical and Applied Mechanics, Siberian Brrulch USSR Academy of Sciences, Novosibirsk 630090

Zhang W. China Beijing Institute of Aerodynamics, Beij ing

Zheltovodov A.A. USSR Inst. of Theoretical and Applied Mechanics, Siberian Branch USSR Academy of Sciences, Novosibirsk 630090

Zhou B. China Beijing University of Aero-nautics and Astronautics, Beij ing 100083

Zlatev P. Bulgaria Bulgarian Ship Hydrodynamic Centre, Varna 9003

Contents

Session 1 Chairman J.L. van Ingen

Dallmann U.

Belotserkovsky O.M. Gushin V.A.

Kovenya V.M. Lebedev A.S. Cherny S.G.

smith F.T.

Bogdanova E.V. Ryzhov O.S.

Ruban A.I.

Hackmueller G. Kluwick A.

session 2 Chairman O.S.Ryzhov

Vojtkova G.V. Lunev V.V.

Black D. W. Rothmayer A.P.

Goldshtik M.A. Shtern V.N.

Belotserkovsky S.M.

Poster session:

Bakker P.G.

Analysis of simulations of topo­logically changing three-dimen-sional separated flows ••••••••.•.. 1

Direct numerical modelling: un­steady separation, coherent structures and transition to chaos •••••.••••••••••••••••••.••.• +)

Numerical simulation of separated flows by the splitting up method

Break-up in steady and unsteady

15

separation •••••••.••••.••.•...••.• 25

On Goldstein's singularity •••••••• 39

Marginal separation theory •..•••.. 47

Effects of 3-D surface mounted obstacles on marginal separation ••• 55

Discontinuous solutions of bound-ary layer equations with positive pressure gradient •••••.•••....•.•• 67

Computation of trailing-edge sep­aration using an accelerated, up­dated bluff-body, interacting boundary-layer algorithm ••.•.•.•.• 77

Self-similar separation •.•.••••••. 89

Digital simulation of separated and jet flows using discrete vor-tex method •••••••••••••••.••..•.•. 97

Topology of fundamental separation structures .•••••..•••.••...•.•.••. 103

Basin M.A.

Borisov A.V. Tarnavsky G.A.

Chernyshenko S.I.

Gourevitch U.G. Shoubin E.B.

Gushchin V.A. Konshin V.N.

Konotop T.V. Trigub V.N.

Korolev G.L.

Lee Ch.-H. Chen Y.-Q. Zhou N.

Miyake Y. Kajishima T.

Panovko M.Ya.

Sadovsky V.S.

Xiong S.W. Feng Y.N. Zheng B.

Schulte-Werning B. Dallmann U.

Sychev victor V.

XIX

Basic equations of vortex fluid motion. Vortex-wave resonance ..... 113

Numerical investigation of turbu­lent separated flows in the near wake after body .................. 117

Asymptotic theory of the station-ary flow around bluff bodies ..... 121

Modeling of the flows with 3-D separation caused by interaction of the boundary layers on the intersecting surfaces ............ 125

Numerical simulation of the sep­arated fluid flows at large Rey-nolds numbers .................... 129

A boundary layer near small three­dimensional roughnesses in a supersonic flow about a cooled body .............•......•........ 133

Interaction theory and non-unique­ness of separated flows around solid bodies ..................... 139

Finite element simulation of un-steady separated flows ........... 143

Explanation of the origin of the secondary flow in a straight square duct on the Basis of LES

Spatial vortex structures and heat transfer in a channel having

149

a step ........................... 153

Some investigation results for vortex-potential inviscid fluid flows ............................ 157

A simulation of the wing leading­edge vortex and its entrainment effect ........................... 161

Numerical simulation of the vor­tex chain formation by vorticity shedding from a sphere into the wake ............................. 167

Asymptotic theory of a flow near the trailing tip of a slender axisymmetric body •..........•.... 171

xx Christov C. I. Todorov M.D.

vasilev V. I. Zakotenko S.N. Krasheninnikov S.Ju.

Xa M. Zi-qiang Z.

session 3 Chairman M.Kiya

Castro I.P.

Gogish L.V. Pinke L.M.

Masuda S. Ooizumi H. Yoshizumi K.

Lu Zhi Yong

Zheltovodov A.A.

Danjkov B.N. Kornienko E.S. Kudrjavtsev V.V.

Horstman C.C.

Settles G.S. Alvi F.S. Hsu J.C.

Knight D.O.

session 4 Chairman F.T.Smith

Bogdonoff S.M.

Brodetskii M.D. Maksimov A. I. Kharitonov A.M.

Numerical solution of 2-D Helm­holtz problem for blunt bodies and airfoils .••••••••...•••...•.. 175

Numerical modeling of 3-D turbu-lent flows in mixers ............. 181

Three-dimensional viscous-invis­cid interactions for turbulent flows with separation .•.•.•...•.. 185

Turbulence in incompressible separated flows •..•••••••..•..•.. 191

separated flows in diffuser ducts 207

structure of turbulent separating flow in two-dimensional diffusor . 209

A study on mode of 3-dimensional separation and open separation ... 217

Peculiarities of development and modelling possibilities of super­sonic turbulent separated flows .• 225

supersonic separation zone pres­sure fluctuations for wide range of Reynolds number ....•.•........ 237

Turbulence modeling for sharp­fin-induced shock wave/turbulent boundary-layer interactions ...... 245

On the shock-bifurcation/jet­impingement structure of swept interactions and related flow-fields .••••.•.•.......•.......... 255

Calculation of 3-D shock wave­turbulent boundary layer inter­actions generated by sharp fins ... 263

F1owfie1d modeling of a three-di­mensional shock wave turbulent boundary layer interaction ....•.. 279

Development of 3-D separated flows by longitudinal supersonic flow over the corner configurations ... 303

Borovoi V.Ya. Brazhko V.N. Maikapar G.I.

Assanin S.N. Butkov A.S. Gorokhov S.A. Lapygin V.I. Lyashkoff V.I.

Poster session

Bartsch P. weiser N. Nitsche W.

Borisov A.V. Zheltovodov A.A. Trofimov V.M. Shileyn E.Kh. Yakovlev V.N.

Bormusov A.A. Glebov G.A. Kozlov A.P.

Brodetsky M.D. Shevchenko A.M.

Vasenev L.G. Kharitonov A.M.

Citavy J. Dushek M.

Doerffer P. Dallmann U.

Dvorak R. Zheltovodov A.A. Maksimov A.I. Safarik P. Shileyn E.Kh.

Glagolev A.I. Zubkov A.I. Lyagushin B.E. Panov Yu.A.

Goldfeld M.A. Lisenkov I.G.

Gugavin A.I. Kirnasov B.S. Korobov Y.P. Kudrjavtsev V.V.

XXI

Leeward separated supersonic flows ........•....•.............. 311

Experimental and numerical studies of separated flows about slender axisymmetrical bodies ..•• 319

Experimental and numerical in­vestigations on turbulent sep-arated diffuser flows .•....•••... 327

Analysis of turbulent separated flows in the vicinity of two-di­mensional obstacles under super-sonic speeds conditions .......... 333

Non-stationary structure at sep­aration and turbulent flow at-tachment zones ................... 337

Some features of a separated flow and supersonic vortex structure at the leeside of a delta wing 341

Separated flow around a delta wing in combination with a body .. 345

Separated flow in a straight compressor cascade ............... 349

Secondary corner and channel flow effects on shock induced turbulent flow separation ......•........... 361

Development of two-dimensional analogies comformably to three-dimensional separated flows ...... 365

Three-dimensional open separation in supersonic flows .............. 369

Investigation of compressible turbulent boundary layer with large adverse pressure gradient

The critical phenomena in separ-

377

ated flows ............•.......... 381

XXII

Khlebnikov V.S.

Kornilov V. I. Mekler O.K.

Korobitsin G.P. Petrov V.A. Chupina S.V.

Li S. Xiaoshen Yu. Nanqian Ch.

Marsik F. Vlcek V.

Paskonov V.M. Artamonova M.S.

Safarik P.

Trofimov V.M. Shtrekalkin S.I.

Voropaev G.A. Ptuha Yu.A.

Zapryagaev V.I. Mironov S.G.

Session 5 Chairman A.Michalke

Lin J.C. Howard F.G. Bushnell O. M. Selby G.V.

Hsing T.O. Zhang Z.Q. Hong J.S. Zhuang F.G.

Leontyev A.I. Epifanov V.M. Pavlyuchenko A.'M. Pashutov A.V. Strel'chenko A.N.

Nonstationary disturbance effect on flow in supersonic separated zones ....••.•.••.••.•••••........ 385

Peculiarities of development of separated and relaxation phenomena behind a cylinder flowed about transversally in a shear flow .•.• 389

Numerical and experimental simula­tion of separated flows •......... 393

Some separation characteristics on the ogive nosed body at supersonic flows .....•.•.•.••••..•.•.....•.• +)

Influence of flow separation on transonic instability •..•....•... 397

Numerical simulation of separated unsteady flows of viscous compres-sible gas .•••.•..•••••..••.•••••. 403

An experimental study of separated flows in transonic blade cascades 411

Longitudinal vortices and heat transfer in reattached shear layer 417

Forming of flow recirculation re­gions on convex-concave surfaces . 421

Supersonic pulsating flow in sep­arated zone of spike-tipped cyl-inder •••......................... 425

Comparative study of control techniques for two-dimensional low-speed turbulent flow sep-aration •.•.•..•.•..••.••.•••.•••. 429

A study of the interaction of separated vortices in transonic and supersonic flow on improving the aerodynamic characteristics of vortex-flap ..•.•..•........... 475

Supersonic turbulent separated flows of three types on a porous surface under air injection condi-tions •.•........•................ 485

Volchkov E.P. Lebedev V.P. Nizovtsev M.I. Terekhov V.I.

Meier G.E.A. Ehrenfried K. Grabitz G. Rein M.

Poster session

Glotov G.F.

Vedernikov Yu.A. Derunov E.K. Fedotov V.G.

Yurchenko N.F.

Kozlov V.V. Lushin V.N. Zanin B.Yu.

Zheltovodov A.A. Yakovlev V.N.

Gimranov E.G.

Session 6

The flow separation from a duct wall caused by the near-wall

XXIII

counterjet ....................... 493

Wave models for unsteady separa-tion and jets •.••.••••......•.•.. 503

Axisymmetrical separated zone control in supersonic flows ...... 513

Using of supersonic flow separa­tion on cylinders with nose needles to decrease their drag

Control of separated laminar boundary layers on surfaces with

517

a concave section ................ 521

Separated flow reattachment at an airfoil under sonic effect ....... 525

Regimes of separated flows in finite-width cavities and methods of their control ...........•..... 529

A jet-turbulent "pseudo-shock" model ............................ 533

Chairman V.Ya.Levchenko

Kozlov V.V.

Van Ingen J.L.

Michalke A.

Boiko A.V. Dovgal A.V. Scherbakov V.A. Simonov O.A.

Sutton E.P. Devenport W.J. Barkey Wolf F.D.

AI-Maaitah A.A. Nayfeh A.H. Ragab S.A.

Laminar separation and stability +)

Research on laminar separation bubbles at Delft University of Technology ..........•............ 537

On the instability of wall­boundary layers close to separa-tion .......................•..... 557

Effects of laminar-turbulent transition in separation bubbles .......................... 565

Experimental studies of the re­attachment of separated shear layers ........................... 573

Effect of heat transfer on the stability of separated subsonic flows down-stream of smooth humps and backward-facing steps ........ 589

XXIV

Hipp-Kalthoff C. Fasel H.

Martin J.E. Meiburg E. Lasheras C.

Kiya M. Mochizuki O. Tanaka H. Tsukasaki T.

session 7

Numerical simulations of two-di­mensional temporal and spatial free shear layers: a comparison 617

Three-dimensional evolution of axisymmetric jets: a comparison between computations and experi-ments •...••.•.•.•..•..•.•••..••.. 629

Control of a turbulent leading-edge separation bubble ........... 647

Chairman M.A.Goldshtik

Leibovich S.

Karavaev E.A. Prudnikov Yu.A. Shumsky G.M.

Zohar Y. Ho C.M.

Werle H.

Sun M. Wang J. Lian Q.

Poster session

Althaus W.

Arnal M. Friedrich R.

Bardakhanov S.P. Larichkin V.V.

Bogolepov V.V. Lipatov r. r.

The local dynamics of vortical flows............................ +)

Self-induced roll-oscillations on lifting systems with flow separation on high angles of attack ........•...•......•.... '" 657

Small eddies in large vortices 665

Hydrodynamic visualization of separated flows and jets ••.•..••• 671

A numerical and experimental study of the starting flow of a uniformly accelerated circular cylinder .•..•••••..•.•.......•.•. 681

Experimental and theoretical investigation of vortex forma-tion in the wake of a flat plate for subsonic and supersonic free-stream Mach number .•........ 691

The instantaneous structure of a turbulent flow over a back­ward-facing step ...•••........... 709

Influence of acoustic disturb-ances on the separation flow characteristics behind two semi­infinite circular cylinders ..••.. 719

Asymptotic analysis of the devel­opment of GOrtler vortices in a fluid boundary layer near a con-cave surface ••.•..•.•..•.•...•... 723

Bychkov N.M. Dikovskaya N.D.

Ivanov A.N. Mikhailov V. I .

Kachanov Yu.S. Tararykin 0.1.

Kiselev V.Ya. Lysenko V.I.

Kosinov A.D. Shevelkov S.G.

Kuibin P.A. Rudyak V.Ya. Veretentsev A.N.

stUcke P. Teipel I.

Suzuki K. Kubota H.

Terentiev E.D.

Zakharenkov M.N.

Zanin B.Yu.

session 8 Chairman Ch.-M.Ho

Hussain F.

Isataev S.I. Tarasov S.B. Toleuov G. Jangunov o.

xxv

separation-transition effects on a cylinder with a screen ......... 729

Features of the unsteady separat­ed flow behind flat plates after a shock wave excitation .......... 733

The development of 3-D separated flows and their influence on the stability and laminar-turbulent transition ....................... 737

The boundary layer turbulization by means of an obstacle at large flow-past velocities ............. +)

Experimental investigation of separation and stability of supersonic laminar boundary layer ...........•...•.•....•..... 741

Processes of the instability development in separated flows behind the plate ................. 747

separation of flow around a circular cylinder at moderate Re-numbers .........•.•........... 751

Computational studies on topo­logical properties of vortex core lines in separated flow field around high-angle-of-at-tack cone-cylinders .•............ 755

stability of separated flow before and after the small step +)

Formation of vortex structures in a viscous incompressible flow past an airfoil ............. 763

Laws of generation of instabil­ity waves in laminar separation of the flow from the airfoil ..... +)

organized structures in jets and mixing layers .................... +)

The investigation of the role of the coherent structures in the development of the three-dimensional jets and wakes ....... 767

XXVI

Krothapalli A. Lourenco L. Shih C.

Comte P. Lesieur M.

Movchan V.T. Mkhitaryan A.M. Shkvar E.A.

Schetz J.A. Thomas R.H. Billig F.S.

Poster session

Albazarov B.Sh. Bezrukov A.A.

Alekseenko S.V. Markovich O.M.

Kislykh V.V. Kudriavtsev V.V. Kulikov V.N. Reshetin LA. Rybak S.P.

Kislykh V.V. Reshetin I.A.

Panov B.F.

Petrunin A.A. Shtern V.N.

Shen G.X.

Sokolov E. L

Suleimanov Sh.

Tang S.K. Ko N.W.M.

Vortex interactions in the transition region of a rectan-gular jet .••••••.....•.....•..... 775

Two manners of becoming three­dimensional for mixing layers .... 785

The simulation of turbulent sep­arated boundary layers and wall jets ...•.•.•••....•..•.•••..•...• 799

Mixing of transverse jets and wall jets in supersonic flow ..... 807

Numerical simulation of supersonic free jet by TVO schemes .......... 839

Interaction of plane, turbulent jets .....•••..................... 843

Parametric analysis of acoustic near field characteristics of supersonic high temperature jet .. 847

Afterbody effects study on Energia reusable launcher models. Selec­tion of jet propulsive masses parameters within jet streams ejecting model ................... 851

Tangential stress on a cylinder surface impinged by a underex-panded low density jet ••......... 855

MHo-jets: collapse and dynamo 859

An experimental investigation in a water channel for the vectoring rectangular jet flows .••.•....... 863

The impingement of a supersonic jet upon the surface .••..•....... 869

Self-oscillations and acoustic radiation at discrete frequency of unbalanced jet •••••.•.•..•.•.• 875

Some behaviours of coherent structures under controlled excitation in coaxial jet of mean velocity ratio of 0.3 ....... 879

Ugriumov E.A.

Wu S.P. Lee Ch.-H.

Javorsky N.I.

Zapryagaev V.I. Solotchin A.V.

An autooscillating regime of supersonic jet interaction

XXVII

with a cavity .•...•.••........... 883

A high-resolution, adaptive-grid finite difference algo-rithm for simulating supersonic jet/external flow interactions ... 887

Appearance of the back flow in the non-selfsimilar swirling jet . 891

Three-dimensional structures of the flow in supersonic underex-pended jet ....................... 895

+) papers not available