Accession Number : ADA310636
Title : Hypersonic Experimental and Computational Capability, Improvement and Validation. Volume 1 (l'Hypersonique experimentale et de calcul - capacite amelioration et validation). Volume 1,
Descriptive Note : Advisory rept.,
Corporate Author : ADVISORY GROUP FOR AEROSPACE RESEARCH AND DEVELOPMENT NEUILLY-SUR-SEINE (FRAN CE)
Personal Author(s) : Saric, William S. ; Muylaert, Jean ; Dujarric, Christian
PDF Url : ADA310636
Report Date : MAY 1996
Pagination or Media Count : 203
Abstract : The results of the phase I effort conducted under AGARD Working Group 18 on Hypersonic Experimental and Computational Capability, Improvement and Validation are presented in this report. A discussion of issues and problems classified into seven topic areas precedes the individual sections on Shock/Boundary-Layer Interactions, Laminar-Turbulent Transition, Rarefield Flow, Real-Gas Effects, Facility Calibration Procedures, Extrapolation to Flight and Hypersonic Test Facilities. Recommendations for future work in these areas is included at the end of each section. Conclusions for the work conducted during the phase II of this Working Group will be presented in Volume II.
Descriptors : *AEROTHERMODYNAMICS, *VISCOUS FLOW, *HYPERSONIC FLOW, *RAREFIED GAS DYNAMICS, HEAT TRANSFER, AERODYNAMIC CONFIGURATIONS, NATO, ABLATION, VALIDATION, SHOCK WAVES, TURBULENT FLOW, TURBULENT BOUNDARY LAYER, VORTICES, COMPUTATIONAL FLUID DYNAMICS, FLOW VISUALIZATION, FLOW FIELDS, WIND TUNNEL TESTS, NONEQUILIBRIUM FLOW, MACH NUMBER, TWO DIMENSIONAL FLOW, BOUNDARY LAYER TRANSITION, HYPERSONIC CHARACTERISTICS, HYPERSONIC FLIGHT, FLOW SEPARATION, LAMINAR FLOW, ENTHALPY, PRESSURE DISTRIBUTION, GAS SURFACE INTERACTIONS, SKIN FRICTION, THERMAL RADIATION, BOUNDARY LAYER FLOW, THREE DIMENSIONAL FLOW, EXTRAPOLATION, LAMINAR BOUNDARY LAYER.
Subject Categories : Aerodynamics
Distribution Statement : APPROVED FOR PUBLIC RELEASE