It was on a proposal of the late Professor Maurice Roy, member of the French Academy of Sciences, that in 1982, the General Assembly of the International Union of Theoretical and Applied Mechanics decided to sponsor a symposium on Turbulent Shear-Layer/Shock-Wave Interactions. This sympo sium might be arranged in Paris -or in its immediate vicinity-during the year 1985. Upon request of Professor Robert Legendre, member of the French Academy of Sciences, the organization of the symposium might be provided by the Office National d'Etudes et de Recherches Aerospatiales (ONERA). The request was very favorably received by Monsieur l'Ingenieur General Andre Auriol, then General Director of ONERA. The subject of interactions between shock-waves and turbulent dissipative layers is of considerable importance for many practical devices and has a wide range of engineering applications. Such phenomena occur almost inevitably in any transonic or supersonic flow and the subject has given rise to an important research effort since the advent of high speed fluid mechanics, more than forty years ago. However, with the coming of age of modern computers and the development of new sophisticated measurement techniques, considerable progress has been made in the field over the past fifteen years. The aim of the symposium was to provide an updated status of the research effort devoted to shear layer/shock-wave interactions and to present the most significant results obtained recently.
Reihe
Auflage
Softcover reprint of the original 1st ed. 1986
Sprache
Verlagsort
Verlagsgruppe
Zielgruppe
Für Beruf und Forschung
Research
Illustrationen
Maße
Höhe: 235 mm
Breite: 155 mm
Dicke: 25 mm
Gewicht
ISBN-13
978-3-642-82772-3 (9783642827723)
DOI
10.1007/978-3-642-82770-9
Schweitzer Klassifikation
Session 1 Interactions in Two-Dimensional Steady Flows Chairman: B.E, Launder.- Modelling of Compressible Turbulent Flows: Present Possibilities and Perspectives (*).- Transonic Separated Flow Prediction Based on a Mathematically Simple, Nonequilibrium Turbulence Closure Model.- Turbulence Modeling in Transonic Interactions.- Implicit Navier-Stokes Calculations of Transonic Shock/Turbulent Boundary-Layer Interactions.- Session 2 Interaction in Two-Dimensional Steady Flows Chairman: H. HaMinh.- Strong versus Weak Interaction System for Transonic Flow Computation.- Application of Interacting Boundary-Layer Theory in the Analysis of Transonic Shock Induced Separation.- The Shock-Wave/Turbulent Boundary-Layer Interaction on Curved Surface at Transonic Speed.- Calculation of 2D Turbulent Shock/Boundary Layer Interaction at Curved Surfaces with Suction and Blowing.- Improvement of Transonic Airfoil Performance through Passive Shock/Boundary-Layer Interaction Control.- Session 3 Interactions in Two-Dimensional Steady Flows Chairman: S.M. Bogdonoff.- Physical Analysis of Turbulent Boundary Layer/ Shock-Wave Interactions Using Second Order Closure Predictions.- Turbulent Properties of Axisymmetric Shock-Wave/Boundary-Layer Interaction Flows.- An Asymptotic Theory of Supersonic Turbulent Interactions in a Compression Corner.- Second Order Computation of Shock-Wave/Boundary-Layer Interactions in Curvilinear Coordinates.- Navier-Stokes and Experimental Modeling of Blunt-Base Rocket Nozzle Flow.- Session 4 Interactions in Three-Dimensional Steady Flows Chairman: E. Krause.- A "Preview" of Three-Dimensional Shock-Wave/ Turbulent Boundary-Layer Interactions(*).- On the Inception Lengths of Swept Shock-Wave/ Turbulent Boundary-Layer Interactions.- Experimental Study of theBoundary-Layer Separation Conditions through a Shock-Wave on Airfoil and Swept Wing.- A Model of the Flow over Swept Wings with Shock Induced Separation.- Separation ahead of Blunt Fins in Supersonic Turbulent Boundary-Layers.- Session 5 Interactions in Three-Dimensional Steady Flows Chairman: H. Fernholz.- Some Observations of Three-Dimensional Shock-Wave/ Turbulent Boundary-Layer Interactions.- Experimental Study of Shock-Wave/Boundary-Layer Interaction in a Three Dimensional Channel Flow.- Numerical Experiment with Inviscid Vortex-Stretched Flow around a Cranked Delta Wing: Transonic Speed.- Supersonic Viscous-Inviscid Interaction of a Swept Compression Ramp with a Turbulent Boundary-Layer.- Shock/Boundary-Layer Interaction Model for Three-Dimensional transonic Flow Calculations.- Aerothermal Problems Associated with Viscous/ Inviscid Interaction over Hypersonic Flight Vehicles.- Session 6 Unsteady Aspects of Interaction Phenomena Chairman: O. Leuchter.- Unsteadiness of Shock-Wave Induced Turbulent Boundary-Layer Separation. A Review(*).- Reduction of Low Frequency Buffet from a Bluff Body at Transonic Speeds.- Turbulence Alteration due to Shock Motion.- Properties of Wall Pressure Fluctuations in a Separated Flow over a Compression Ramp.- A Shock-Wave/Free Turbulence Interaction.- Session 7 Other Aspects of Interaction Flows Chairman: O. Leuchter.- An Overview of some Investigations of Pressure and Thermal Distributions Induced by Trailing Edge Controls on Hypersonic Aircraft.- Fluid Turbulence: Deterministic or Statistical.
