Symposium Transsonicum III -

Symposium Transsonicum III

IUTAM Symposium Göttingen, 24.–27.5.1988

Jürgen Zierep, H. Oertel (Herausgeber)

Buch | Softcover
XIX, 504 Seiten
2011 | 1. Softcover reprint of the original 1st ed. 1989
Springer Berlin (Verlag)
978-3-642-83586-5 (ISBN)
106,99 inkl. MwSt
Continuing the tradition of the IUTAM Symposia TRANSSONICA, this review of the numerical simulation and physical modelling of transonic flows presents new developments in the fields of computational and experimental aerodynamics. A major topic of the symposium proceedings is the evaluation of present numerical analysis techniques with respect to transonic aerodynamics. In the field of experimental aerodynamics, the high Reynolds number effect and the interference-free testing in transonic wind tunnels are of special interest.

Prof. em. Dr.-Ing. Dr. techn. E. h. Dr. h. c. Jürgen Zierep hatte den Lehrstuhl für Strömungslehre an der Technischen Universität in Karlsruhe inne und ist Honorarprofessor an der BUAA (Beijing University for Aeronautics and Astronautics).

Session 1 CFD - Applications.- Summary and Evaluation of the Workshop "Numerical Simulation of Compressible Viscous-Flow Aerodynamics".- Use of CFD and Experiment in Transonic Aircraft Design.- Computational Transonic Aerodynamics Research in Japan.- Viscous-Inviscid Strategy and Computation of Transonic Buffet.- Zonal Solutions of Three-Dimensional Viscous Flow Problems.- On the Computation of Transonic Viscous Flows.- Improvements in the Formulation and Numerical Solution of the Euler Problem for Swept Wings.- Transonic Computations by Multidomain Techniques with Potential and Euler Solvers.- On the Development and Application of Software based on the Framework of Cartesian Coordinates.- Numerical Simulation and Physical Modelling of Transonic Trailing Edge Flow.- Theoretical and Experimental Investigation of 2-D Diabatic Transonic and Supersonic Flow Fields.- Session 2 Asymptotics and Theory.- Asymptotic Methods in Transonic Flow Theory.- Some Asymptotic Problems of Transonic Flow Theory.- Transonic Degeneracy in Systems of Conservation Laws.- Transonic Equivalence Rule: Unresolved Aspects of Asymptotic and CFD Studies.- Perturbation Analysis of Unsteady Transonic Flow through Cascades.- Viscous Transonic Flow in the Vicinity of a Corner Point.- Session 3 Stability and Transition.- Stability of Three-Dimensional Boundary Layers on Swept Wings at Transonic Speeds.- Transition Prediction in External Flows via Linear Stability Theory.- Theoretical Investigation of Instability and Transition in the DFVLR-F5 Swept-Wing Flow.- Transition Prediction in Transonic Flow.- Session 4 Vortical Flows.- Transonic Vortical Flow.- Experimental Study on Vortex and Shock Wave Development on a 65° Delta Wing.- Computations Relating to the Vortex Flow Experiment.- Navier-Stokesand Euler Solutions for Vortex Flow over a Delta Wing.- Computation of Vortex Flow on a Delta Wing at Transonic Speed.- Vortical Flows on the Lee Surface of Delta Wings.- Numerical Simulation of Rotational Flows.- Session 5 Turbulent Shock - Boundary Layer Interaction.- Recent Basic Studies on Transonic Shock-Wave/Turbulent Boundary-Layer Interactions.- Passive Control of Transonic Shock/Boundary Layer Interaction.- Turbulent Shock - Boundary-Layer Interaction with Control Theory and Experiment.- Passive Control of Shock - Boundary-Layer Interactions: Numerical and Experimental Studies.- Transonic Inviscid-Viscous Interactions over Porous Surfaces.- Wind Tunnel Studies of Natural Shock Wave - Separation Instabilities for Transonic Airfoil Tests.- Three-Dimensional Flow Separation caused by Normal Shock-Wave / Turbulent Boundary-Layer Interaction.- Session 6 Unsteady Flows.- Unsteady Phenomena.- Unsteady Aeroelastic Computations for Flexible Configurations at Transonic and Supersonic Speeds.- Mechanism and Reynolds Number Dependence of Shock-Induced Buffet on Transonic Airfoils.- Computational and Experimental Research on Buffet Phenomena of Transonic Airfoils.- Concluding Remarks.

Erscheint lt. Verlag 5.12.2011
Reihe/Serie IUTAM Symposia
Zusatzinfo XIX, 504 p.
Verlagsort Berlin
Sprache englisch
Maße 155 x 235 mm
Gewicht 790 g
Themenwelt Naturwissenschaften Physik / Astronomie Mechanik
Schlagworte aerodynamics • aircraft design • CFD • Design • Development • Dynamics • Natur • Simulation • Software
ISBN-10 3-642-83586-4 / 3642835864
ISBN-13 978-3-642-83586-5 / 9783642835865
Zustand Neuware
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