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Titolo: |
Thermophysical aspects of re-entry flows [[electronic resource] /] / edited by James N. Moss, Carl D. Scott
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Pubblicazione: | New York, N.Y., : American Institute of Aeronautics and Astronautics, Inc., c1986 |
Descrizione fisica: | 1 online resource (636 p.) |
Disciplina: | 629.1 s |
629.4/152 | |
Soggetto topico: | Space vehicles - Atmospheric entry |
Aerothermodynamics | |
Aerodynamics, Hypersonic | |
Soggetto genere / forma: | Electronic books. |
Altri autori: |
MossJames N
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Note generali: | "Technical papers selected from the AIAA 23rd Aerospace Sciences Meeting, January 1985, and the AIAA 20th Thermophysics Conference, June 1985, and subsequently revised." |
Nota di bibliografia: | Includes bibliographical references and index. |
Nota di contenuto: | ""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 Air""""Electron-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 Heating""""Measured 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 Flow""""Convergence 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"" | |
Titolo autorizzato: | Thermophysical aspects of re-entry flows ![]() |
ISBN: | 1-60086-577-1 |
1-60086-358-2 | |
Formato: | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione: | Inglese |
Record Nr.: | 9910457232503321 |
Lo trovi qui: | Univ. Federico II |
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