Thermophysical aspects of re-entry flows /

Detalles Bibliográficos
Clasificación:Libro Electrónico
Autores Corporativos: American Institute of Aeronautics and Astronautics, AIAA Aerospace Sciences Meeting, AIAA Thermophysics Conference
Otros Autores: Moss, James N., Scott, Carl D.
Formato: Electrónico Congresos, conferencias eBook
Idioma:Inglés
Publicado: New York, N.Y. : American Institute of Aeronautics and Astronautics, ©1986.
Colección:Progress in astronautics and aeronautics ; v. 103.
Temas:
Space vehicles > Atmospheric entry.
Aerothermodynamics.
Aerodynamics, Hypersonic.
Véhicules spatiaux > Entrée dans l'atmosphère.
Aérothermodynamique.
Aérodynamique hypersonique.
Aerodynamics, Hypersonic
Aerothermodynamics
Space vehicles > Atmospheric entry
Acceso en línea:Texto completo
Tabla de Contenidos:
  • Cover
  • Title
  • Copyright
  • Table of Contents
  • Preface
  • Editorial Committee
  • Chapter I. Low-Density Phenomena
  • Low-Density Aerothermodynamics
  • Direct Simulation Monte Carlo Method and Comparison with Experiment
  • Drag of Bodies in Rarefied Hypersonic Flow
  • Heat Transfer on a Flat Plate in Continuum to Rarefied Hypersonic Flows at Mach 19.2 and 25.4
  • Transitional, Hypervelocity Aerodynamic Simulation and Scaling
  • Gas/Surface Scattering Models for Satellite Applications
  • Chapter II. High Temperature Kinetics and Transport Properties
  • Rate Constants for Chemical Reactions in High-Temperature Nonequilibrium AirElectron-Nitrogen Molecule Collisions in High-Temperature Nonequilibrium Air
  • Electron-Impact Vibrational Excitation Rates in the Flowfield of Aeroassisted Orbital Transfer Vehicles
  • Theoretical Studies of Dissociative Recombination
  • N+ -N and 0+ -0 Interaction Energies, Dipole Transition Moments, and Transport Cross Sections
  • Transport Properties for Some Atom/Ion Interactions in Air
  • Chapter III. Aerothermodynamic Ground Simulations and Measurements
  • Studies of Potential Fluid-Mechanical Mechanisms for Enhanced Stagnation-Region HeatingMeasured and Predicted Vortex-Induced Leeward Heating on a Biconic at Mach 6 and 10
  • Heating Rate Distributions at Mach 10 on a Circular-Body Earth-to-Orbit Transport Vehicle
  • Developments in Aerothermal Test Techniques at the AEDC Supersonic/Hypersonic Wind Tunnels
  • Application of Numerical Simulation to Enhance Arcjet Performance
  • Effects of Surface Discontinuities on Convective Heat Transfer in Hypersonic Flow
  • Chapter IV. Numerical Simulations of Hypersonic Flows
  • Chemical and Thermal Nonequilibrium Heat-Transfer Analysis for Hypervelocity, Low Reynolds Number FlowConvergence of Computation of Chemical Reacting Flows
  • Radiative Viscous Shock Layer Analysis of Fire, Apollo, and PAET Flight Data
  • Three-Dimensional Viscous Shock Layer Applications for the Space Shuttle Orbiter
  • Numerical Simulation of Hypersonic Viscous Fore- and Afterbody Flows over Capsule-Type Vehicles at Angles of Attack
  • Two Dimensional and Axisymmetric Heat-Transfer Results with the CSCM Upwind Implicit Algorithm
  • Author Index

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