Thermophysical aspects of re-entry flows [[electronic resource] /] / edited by James N. Moss, Carl D. Scott |
Pubbl/distr/stampa | 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 |
Altri autori (Persone) |
MossJames N
ScottCarl D |
Collana | Progress in astronautics and aeronautics |
Soggetto topico |
Space vehicles - Atmospheric entry
Aerothermodynamics Aerodynamics, Hypersonic |
Soggetto genere / forma | Electronic books. |
ISBN |
1-60086-577-1
1-60086-358-2 |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
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"" |
Record Nr. | UNINA-9910457232503321 |
New York, N.Y., : American Institute of Aeronautics and Astronautics, Inc., c1986 | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Federico II | ||
|
Thermophysical aspects of re-entry flows [[electronic resource] /] / edited by James N. Moss, Carl D. Scott |
Pubbl/distr/stampa | 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 |
Altri autori (Persone) |
MossJames N
ScottCarl D |
Collana | Progress in astronautics and aeronautics |
Soggetto topico |
Space vehicles - Atmospheric entry
Aerothermodynamics Aerodynamics, Hypersonic |
ISBN |
1-60086-577-1
1-60086-358-2 |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
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"" |
Record Nr. | UNINA-9910781700603321 |
New York, N.Y., : American Institute of Aeronautics and Astronautics, Inc., c1986 | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Federico II | ||
|
Thermophysical aspects of re-entry flows [[electronic resource] /] / edited by James N. Moss, Carl D. Scott |
Pubbl/distr/stampa | 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 |
Altri autori (Persone) |
MossJames N
ScottCarl D |
Collana | Progress in astronautics and aeronautics |
Soggetto topico |
Space vehicles - Atmospheric entry
Aerothermodynamics Aerodynamics, Hypersonic |
ISBN |
1-60086-577-1
1-60086-358-2 |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
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"" |
Record Nr. | UNINA-9910818946003321 |
New York, N.Y., : American Institute of Aeronautics and Astronautics, Inc., c1986 | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Federico II | ||
|