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Hypersonic Flow Research.

Detalles Bibliográficos
Clasificación:Libro Electrónico
Autor principal: Riddell, Frederick R.
Formato: Electrónico eBook
Idioma:Inglés
Publicado: Reston : American Institute of Aeronautics and Astronautics, 2000.
Temas:
Acceso en línea:Texto completo
Tabla de Contenidos:
  • ""Cover""; ""Title""; ""Copyright""; ""Hypersonics Committee""; ""Preface""; ""Contents""; ""The ARS â€? AFOSR International Hypersonics Conference: Summary and Comments""; ""A. Hypersonic Flow at Low Reynolds Number""; ""Introduction""; ""Density Behavior along the Stagnation Line of a Blunt Body in Hyperthermal Flow""; ""Second-Order Compressible Boundary Layer Theory with Application to Blunt Bodies in Hypersonic Flow""; ""Comment on above paper""; ""Rarefied Hypersonic Flow over a Sphere""; ""The Rayleigh Problem for a Dissociated Gas""; ""B. Chemical Kinetic Effects in Hypersonic Flow""
  • ""Introduction""""Chemical Kinetics: A General Introduction""; ""Chemical Kinetics of High Temperature Air""; ""Chemical Effects in External Hypersonic Flows""; ""Radiation at Hypersonic Speeds""; ""Radiation from the Nonequilibrium Shock Front""; ""C. Inviscid Hypersonic Flow""; ""Introduction""; ""Slender Wings at High Angles of Attack in Hypersonic Flows""; ""Newtonian Theory of Hypersonic Flow at Large Distances from Bluff Axially Symmetric Bodies""; ""Shock Layer Structure and Entropy Layers in Hypersonic Conical Flows""; ""Theory of Entropy Layers and Nose Bluntness in Hypersonic Flow""
  • ""D. Experimental Techniques I""""Introduction""; ""Aerodynamic Testing at Mach Numbers from 15 to 20""; ""The Duration and Properties of the Flow in a Hypersonic Shock Tunnel""; ""An Evaluation of the Hypersonic Gun Tunnel""; ""Diagnostic Studies of a Low Density, Arc Heated Wind Tunnel Stream""; ""Initial Results from a Low Density, Hypervelocity Wind Tunnel""; ""E. Experimental Techniques II""; ""Introduction""; ""The Free Flight Range: A Tool for Research in the Physics of High Speed Flight""; ""Survey of Shock Tube Research Related to the Aerophysics Problem of Hypersonic Flight""