| Description |
1 online resource (xv, 620 pages) : illustrations |
| Series |
Progress in astronautics and aeronautics ; v. 103 |
|
Progress in astronautics and aeronautics ; v. 103.
|
| Contents |
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 |
| Notes |
"Technical papers selected from the AIAA 23rd Aerospace Sciences Meeting, January 1985, and the AIAA 20th Thermophysics Conference, June 1985, and subsequently revised." |
| Bibliography |
Includes bibliographical references and index |
| Subject |
Space vehicles -- Atmospheric entry.
|
|
Aerothermodynamics.
|
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Aerodynamics, Hypersonic.
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Aerodynamics, Hypersonic
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Aerothermodynamics
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Space vehicles -- Atmospheric entry
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| Form |
Electronic book
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| Author |
Moss, James N
|
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Scott, Carl D
|
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American Institute of Aeronautics and Astronautics.
|
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AIAA Aerospace Sciences Meeting (23rd : 1985 : Reno, Nev.)
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AIAA Thermophysics Conference (20th : 1985 : Williamsburg, Va.)
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| LC no. |
86010807 |
| ISBN |
9781600863585 |
|
1600863582 |
|
