Turbulent Shear-Layer/Shock-Wave Interactions: IUTAM Symposium, Palaiseau, France September 9–12, 1985: International Trends in Manufacturing Technology
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Specificații
ISBN-13: 9783642827723
ISBN-10: 3642827721
Pagini: 460
Ilustrații: XXV, 430 p.
Dimensiuni: 155 x 235 x 24 mm
Greutate: 0.64 kg
Ediția:Softcover reprint of the original 1st ed. 1986
Editura: Springer Berlin, Heidelberg
Colecția Springer
Seria International Trends in Manufacturing Technology
Locul publicării:Berlin, Heidelberg, Germany
ISBN-10: 3642827721
Pagini: 460
Ilustrații: XXV, 430 p.
Dimensiuni: 155 x 235 x 24 mm
Greutate: 0.64 kg
Ediția:Softcover reprint of the original 1st ed. 1986
Editura: Springer Berlin, Heidelberg
Colecția Springer
Seria International Trends in Manufacturing Technology
Locul publicării:Berlin, Heidelberg, Germany
Public țintă
ResearchCuprins
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.