New Results in Numerical and Experimental Fluid Mechanics V: Contributions to the 14th STAB/DGLR Symposium Bremen, Germany 2004 PDF
Preview New Results in Numerical and Experimental Fluid Mechanics V: Contributions to the 14th STAB/DGLR Symposium Bremen, Germany 2004
92 Notes on Numerical Fluid Mechanics and Multidisciplinary Design (NNFM) Editors E.H. Hirschel/Miinchen W. Schroder/Aachen K. Fujii/Kanagawa W. Haasc/Miinchen B, van Leer/Ann Arbor M. A. Leschziner/London M. Pandolfi/Torino J. Periaux/Paris A. Rizzi/Stockholm B. Roux/Marseille New Results in Numerical and Experimental Fluid Mechanics V Contributions to the 14th STAB/DGLR Symposium Bremen, Germany 2004 Hans-Josef Rath Carsten Holze Hans-Joachim Heinemann Rolf Henke Heinz Honlinger (Editors) Springer Prof. Dr. Hans-Josef Rath Roff Henke C^arsteii Holze Airbus Deutschland GmbH ZARM - University of Brenien Senior Project Manager Ani Fallturm/Hochiichulring Iliinefeldstraffe 1-5 D-28359 Bremen D~28i99 Bremen Dr. Hans-]oachim Heinemaim Professor Dr. Heinz Honlinger Co-Managing Editor DLR - AE ..Aerospace Science and Technology, AST" Bunsenstrafie 10 DLR D-37073 Gottingen BunsenstraCe 10 D-37073 Gottingen Library of Congress Control Number: 2006923556 ISBN-10 3-540-33286-3 Springer Berlin Heidelberg New York ISBN-13 978-3-540-33286-2 Springer Berlin Heidelberg New York This work is subject to copyright. 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Final processing by PTP-Berlin Protago-T£X-Production GmbH, Germany (wtvw.ptp-berlin.com) Cover-Design: deblik, Berlin Printed on acid-free paper 89/3141/Yu - 5 4 3 2 1 0 NNFM Editor Addresses Prof. Dr. Ernst Heinridi Hirschel Prof. Dr. Maurizio Pandolfi (General editor) Politecnico di Torino Herzog-Heinrich-Weg 6 Dipartimento di Ingegneria 0-85604 /.orneding Aeronautica e Spaziale Germany Corso Duca degli Abruzzi, 24 E-mail: [email protected] I-10129 Torino Italy li-mail: [email protected] Prof. Dr. Kozo Fujii Space Transportation Research Division Prof. Dr. Jacques Pcriaux The Institute of Space Dassault Aviation and Aslronaulical Science 78, Quai Marcel Dassault 3-1-1, Yoshinodai, Sagamihara F-92552 St. Cloud Cedex Kanagawa, 229-8510 France Japan E-mail: [email protected] E-mail: fujii(Sflab.eng.isas.jaxa.jp Prof. Dr. Arthur Rizzi Department of Aeronautics Dr. Werner Haase KTH Royal Institute of Technology Holienkircliener Str. I9d Tcknikringcn 8 D-85662 Holienbrunn S-10044 Stockholm Germany Sweden Fi-mail: [email protected] E-mail: [email protected] Prof. Dr. Bram van Leer Dr. Bernard Roux Department of Aerospace Engineering L3M - IMT La Jetee The University of Michigan Technopole de Chateau-Giombert Ann Arbor, MI 48109-2140 F-13451 Marseille ("edex 20 USA France E-mail: bram@ engin.umich.edu E-mail: broux@ I3m.univ-mrs.fr ProL Dr. Yurii I. Sliokin Prof. Dr. Michael A. Leschziner Siberian Branch of the Imperial College of Science Russian Academy of Sciences Technology and Medicine Institute of Computational Aeronautics Department Technologies Prince Consort Road Ac. Lavrentyeva Ave. 6 London SW72BY 630090 Novosibirsk U.K. Russia E-mail: mike.leschziner@ ic.ac.uk E-mail: [email protected] FOREWORD This volume contains the paper presented at the 14* DGLR/STAB- Symposium held at the ZARM, Universitat Bremen, Germany, November, 16 to 18, 2004. STAB is the German Aerospace Aerodynamics Associa tion, founded towards the end of the 1970's, whereas DGLR is the German Society for Aeronautics and Astronautics (Deutsche Gesellschaft fiir Luft- und Raumfahrt - Lilienthal Oberth e.V.). The mission of STAB is to foster development and acceptance of the dis cipline "Aerodynamics" in Germany. One of its general guidelines is to concentrate resources and know-how in the involved institutions and to avoid duplication in research work as much as possible. Nowadays, this is more necessary than ever. The experience made in the past makes it easier now, to obtain new knowledge for solving today's and tomorrow's prob lems. STAB unites German scientists and engineers from universities, re search-establishments and industry doing research and project work in numerical and experimental fluid mechanics and aerodynamics for aero space and other applications. This has always been the basis of numerous common research activities sponsored by different funding agencies. Since 1986 the symposium has taken place at different locations in Ger many every two years. In between STAB workshops regularly take place at the DLR in Gottingen. The changing meeting places were established as focal points in Germany's Aerospace Fluid Mechanics Community for a continuous exchange of scientific results and their discussion. Moreover, they are a forum where new research activities can be presented, often re sulting in new commonly organised research and technology projects. It is the fifths time now that the contributions to the Symposium are pub lished after being subjected to a peer review. The material highlights the key items of integrated research and development based on fruitful col laboration of industry, research establishments and universities. Some of the contributions still present results from the "Luftfahrtforschungspro- gramm der Bundesregierung (German Aeronautical Research Pro gramme)". Some of the papers report on work sponsored by the Deutsche Forschungsgemeinschaft (DFG, German Research Council) in some of their Priority Programs (Verbundschwerpunkt-Programm) as well as in their Collaborative Research Centres (Sonderforschungsbereiche). Other articles are sponsored by the European Community and are therefore re sults of cooperation among different organisations. The main areas include VIII Foreword numerical simulation and mathematics, aeroelasticity, small and large as pect ratio wings in the context of leading-edge vortices, wake vortices, high lift systems and propulsion integration, and new developments in wind tunnel facilities and measurement techniques. Therefore, this volume gives an almost complete review of the ongoing aerodynamics research work in Germany. The order of the papers in this book corresponds closely to that of the sessions of the Symposium. The Review-Board, partly identical with the Program-Committee, con sisted of A. Altminus (Munchen), G. Ashcroft (Koln), J. Ballmann (Aa chen), R. Behr (Munchen), Chr. Breitsamter (Miinchen), A. D'Alascio (Miinchen), J. Delfs (Braunschweig), G. Eitelberg (Emmeloord), M. Fischer (Bremen), R. Friedrich (Munchen), R. Grundmann (Dresden), A. Gulhan (Koln), H. Hansen (Bremen) , S. Haverkamp (Aachen), St. Hein (Gottingen), P. Hennig (UnterschleiBheim), F. Holzapfel (WeBling), H. Honlinger (Gottingen), G. Koppenwallner (Katlenburg-Lindau), W. Kordulla (Noordwijk), H. Komer (Braunschweig), E. Kramer (Stuttgart), H.-P. Kreplin (Gottingen), N. Kroll (Braunschweig), D. Kroner (Frei burg), J. Longo (Braunschweig), Th. Lutz (Stuttgart), F. Menter (Otter- fing), E. Meyer (Munchen), C. Naumann (Stuttgart), G. Neuwerth (Aachen), W. Nitsche (Berlin), H. Olivier (Aachen), R. Radespiel (Braunschweig), H.-J. Rath (Bremen), U. Rist (Stuttgart), H. Rosemann (Gottingen), R. Schnell (Koln), G. Schrauf (Bremen), W. Schroder (Aachen), D. Schwambom (Gottingen), J. Sesterhenn (Munchen), E. Steinhardt (Munchen), Chr. Stemmer (Dreseden), P. Thiede (Bremen), J. Thorbeck (Berlin), C. Tropea (Darmstadt), R. VoB (Gottingen), C. Wagner (Gottingen), C. Weiland (Munchen), C. Weishaupl (Munchen), and W. Wiirz (Stuttgart). Nevertheless, the authors sign responsible for the contents of their contributions. The editors are grateful to Prof. Dr. E. H. Hirschel as the General Editor of the "Notes on Numerical Fluid Mechanics and Muhidisciplinary Design" and to the Springer-Verlag for the opportunity to publish the results of the Symposium. H.-J. Rath, Bremen C. Holze, Bremen H.-J. Heinemann, Gottingen R. Henke, Bremen H. Honlinger, Gottingen October 2005 CONTENTS Page High Aspect-Ratio Wings D. RECKZEH, H. HANSEN: High Reynolds-Number Windtunnel Testing fortheDesignof Airbus Higli-Lift Wings 1 S. MELBER-WILKENDING, G. SCHRAUF, M. RAKOWITZ: Aerodynamic Analysis of Flows with Low Macit and Reynolds-Number under Consideration and Forecast of Transition on the Example of a Glider 9 H. VOLLMERS, W. PUFFERT-MEISSNER, A. SCHRODER: Analysis of PIV Flow Measurements behind the ALVAST-Model in High-Lift Configuration ..17 C. BELLASTRADA, CHR. BREITSAMTER: Effect of Differential Flap Settings on the Wake Vortex Evolution of Large Transport Aircraft 25 S. KAUERTZ, G. NEUWERTH, R. SCHOLL: Investigations on the Influence of Fins on the Extended Nearfield of a Wing in High-Lift Configuration 33 U. HENNE: Application of the PSP Technique in Low Speed Wind Tunnels ... 41 A. GROTE, R. RADESPIEL: Investigation of Tailplane Stall for a Generic Transport Aircraft Configuration 50 TH. STREIT, A. RONZHEIMER, A. BUSCHER: Numerical Analysis of Transport Aircraft Using Different Wing Tip Devices 59 H. STRtJBER, M. HEPPERLE: Aerodynamic Optimisation of a Flying Wing Transport Aircraft 69 Low Aspect-Ratio Wings A. FURMAN, CHR. BREITSAMTER: Delta Wing Steady Pressure Investigations for Sharp and Roimded Leading Edges 77 A. ALLEN, M. D\.TROU, A. PECHLOFF, B. LASCHKA: Computation of Delta Wing Flap Oscillations with a Reynolds-Averaged Navier-Stokes Solver 85 A. SCHMID, CHR. BREITSAMTER: Experimental study on the Flowfield of a Delta-Canard-Configuration with Deflected Leading Edge 94 X Contents Contents (continued) Page A. SCHUTTE, G. EINARSSON, B. SCHONING, A. RAICHLE, TH. ALRUTZ, W. MONNICH, J. NEUMANN, J. HEINECKE: Numerical Simulation of Maneuvering Combat Aircraft 103 B. GOLLING, O. ERIsfE: Experimental Investigation on Periodic Rolling of a Delta Wing Flow at Transonic Mach Numbers 112 U. HERRMANN: Numerical Design of a Low-Noise High-Lift System for a Supersonic Aircraft 120 Helicopters F. LE CHUITON: Chimera Simulation of a Complete Helicopter with Rotors as Actuator Discs 128 A. RAICHLE: Extension of the Unstructured TAU-Code for Rotating Flows .. 136 A. STUERMER: Unsteady Euler and Navier-Stokes Simulations of Propellers with the Unstructured DLR TAU-Code 144 S. MELBER-WILKENDING: Aerodynamic Analysis of Jet-Blast Using CFD Considering as Example a Hangar and an AIRBUS A3 80 Configu^tion 152 Bluff Bodies R. ADELI, J.M.A. LONGO, H. EMUNDS: Flow Field Study of a Supersonic Jet Exiting into a Supersonic Stream 160 K.V. KLINKOV, A. ERDI-BETCHI, M. REIN: Behaviour of Supersonic Overexpanded Jets Impinging on Plates 168 A. KOVAR, E. SCHOLEIN: Study of Supersonic Flow Separation Induced by a Side Jet and its Control 176 J. SRULIJES, F. SEILER: Analytically Obtained Data Compared with Shock Tunnel Heat Flux Measurements at a Conical Body at M = 6 184 Contents XI Contents (continued) Page Laminar Flow Control and Transition A. KRUMBEE^I: Navier-Stokes Airfoil Computations with Automatic Transition Prediction using the DLR TAU Code - A Sensitivity Study 192 J. WILD, O.T. SCHMIDT: Prediction of Attachment Line Transition for a High-Lift Wing Based on Two-Dimensional Flow Calculations with RANS- Solver 200 R. WOKOECK, A. GROTE, N. KRIMMELBEIN, J. ORTMANNS, R. RADESPIEL, A. KRUMBEIN: RANS Simulation and Experiments on the Stall Behaviour ofaTailplane Airfoil 208 I. HOEFENER, W. NITSCHE, A. CARNARIUS, F. THIELE: Experimental and Numerical Investigations of Flow Separation and Transition to Turbu lence in an Axisymmetric Diflfuser 217 I. PELTZER, W. NITSCHE: In-Flight and Wind Tunnel Investigations of Instabilities on a Laminar Wing Glove 225 O. MARXEN, U. RIST, D. HENNINGSON: Steady Three-Dimensional Streaks and their Optimal Growth in a Laminar Separation Bubble 233 T. HETSCH, U. RIST: Applicability and Quality of Linear Stability Theory and Lmear PSE in Swept Laminar Separation Bubbles 241 Active Flow Control A. BRUNN, W. NITSCHE: Drag Reduction of an Ahmed Car Model by Means of Active Separation Control at the Rear Vehicle Slant 249 R. PETZ, W. NITSCHE, M. SCHATZ, F. THIELE: Increasing Lift by Means of Active Flow Control on the Flap of a Generic High-Lift Configuration... 257 P. SCHOLZ, J. ORTMANNS, C.J. KAHLER, R. RADESPIEL: Influencing the Mixing Process in a Turbulent Boimdaiy Layer by Pulsed Jet Actuators .. 265 B. GOKSEL, I. RECHENBERG: Active Flow Control by Surface Smooth Plasma Actuators 273 XII Contents Contents (continued) Page Hypersonic Flows M. HAVERMANN, F. SEILER: Boundary Layer Influence on Supersonic Jet/Cross-Flow Interaction in Hypersonic Flow 281 A. MACK, M. EMRAN, R. SCHAf'ER: Numerical rebuilding of a Generic Body-Flap Model in an Arc Heated Facility 289 U. GAISBAUER, H. KNAUSS, N. N. Fedorova, Y. V. Kharlamova: Experimental and Numerical Investigations of Shock/Turbulent Boundary- Layer Interaction on a Double Ramp Configuration 297 H. LUDEKE, A. FILIMON: Time Accurate Simulation of Turbulent Nozzle FlowbytheDLRTAU-Code 305 ST. LOHLE, M. FERTIG, M. AUWETER-KURTZ: Quantitative Compari son of Measured and Nimierically Simulated Erosion Rates of SiC Based Heat Shield Materials 313 O. BOZIC, J.M.A. LONGO, P. GIESE, J. BEHRENS: High-End Concept to Launch Micro-Satellites into Low-Earth-Orbit Based on Combination of a Two-Stage Rocket and a Railgun-System 322 Aeroelasticity A. SODA, T. TEFY, R. V06: Numerical Simulation of Steady and Unsteady Aerodynamics of the WIONA (Wing with Oscillating Nacelle) Configu ration 330 R. V06, C. HIPPE: Computation of the Flutter Boundary of the NLR 7301 Airfoil in the Transonic Range 338 Aeroacoustics M. FISCHER, H. BIELER, R. EMUNDS: The Noise Criteria within Multidisciplinary High-Lift Design 348 J. ORTMANN, J. WILD: Effect of Noise Reducing Modifications of the Slat on Aerodynamic Properties of the High-Lift System 357
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