Vai al contenuto principale della pagina

Thermophysical aspects of re-entry flows [[electronic resource] /] / edited by James N. Moss, Carl D. Scott



(Visualizza in formato marc)    (Visualizza in BIBFRAME)

Titolo: Thermophysical aspects of re-entry flows [[electronic resource] /] / edited by James N. Moss, Carl D. Scott Visualizza cluster
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  
ScottCarl D  
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  Visualizza cluster
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
Opac: Controlla la disponibilità qui
Serie: Progress in astronautics and aeronautics ; ; v. 103.