Accession Number : ADA267032


Title :   Theoretical and Experimental Methods in Hypersonic Flows (Les Methodes Theoriques et Experimentales pour l'Etude Des Ecoulements Hypersoniques)


Corporate Author : ADVISORY GROUP FOR AEROSPACE RESEARCH AND DEVELOPMENT NEUILLY-SUR-SEINE (FRANCE)


Full Text : https://apps.dtic.mil/dtic/tr/fulltext/u2/a267032.pdf


Report Date : Apr 1993


Pagination or Media Count : 575


Abstract : Major topics covered by the Symposium were testing techniques and instrumentation, computational methods and physical modeling, and validation and accuracy assessment. The sessions were: (1) Design of Hypersonic Vehicle; (2) Facilities;(3) Instrumentation; (4) CFD Validation and Data Accuracy; (5) Rarefied Gas; Real Gas; Chemistry; (6) Boundary Layer Transition; (7) High Enthalpy Nozzle Computation; (8) Development and Application of Code


Descriptors :   *AERODYNAMIC CHARACTERISTICS , *FLUID DYNAMICS , *HYPERSONIC VEHICLES , *HYPERSONIC FLOW , TEST AND EVALUATION , HEAT TRANSFER , COMPUTER PROGRAMS , REENTRY VEHICLES , NATO , SYMPOSIA , SPACECRAFT , AIRCRAFT , MODELS , AERODYNAMIC STABILITY , REPORTS , TURBULENT FLOW , VORTICES , FLOW VISUALIZATION , AIRFOILS , GAS DYNAMICS , RAMJET ENGINES , PIPE FLOW , GAS FLOW , TURBOMACHINERY , NOZZLE GAS FLOW , WIND TUNNELS , TEST FACILITIES , ENTHALPY , BOUNDARY LAYER TRANSITION , PARACHUTES


Subject Categories : Aerodynamics
      Fluid Mechanics
      Thermodynamics
      Spacecraft Trajectories and Reentry


Distribution Statement : APPROVED FOR PUBLIC RELEASE