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Prediction and validation technologies of aerodynamic force and heat for hypersonic vehicle design / / Min Zhao
Prediction and validation technologies of aerodynamic force and heat for hypersonic vehicle design / / Min Zhao
Autore Zhao Min
Edizione [1st ed. 2021.]
Pubbl/distr/stampa Singapore : , : Springer, , [2021]
Descrizione fisica 1 online resource (XIV, 247 p. 149 illus., 89 illus. in color.)
Disciplina 629.132306
Collana Springer aerospace technology
Soggetto topico Aerodynamics, Hypersonic
ISBN 981-336-526-9
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Nota di contenuto Development of Hypersonic Aerothermodynamic Technologies -- An Overview of Ground-Flying Calibration Technologies for Hypersonic Vehicle -- Flow over Blunt Body and Drag Reduction Control -- A Functional Based Prediction Method for Hypersonic Aerodynamic Force and Heat -- Numerical Method for Flow Transition Prediction -- Embedded Aerosphere Sensing System -- Advanced Wind Tunnel Measurement Technology. .
Record Nr. UNINA-9910484868003321
Zhao Min  
Singapore : , : Springer, , [2021]
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Thermophysical aspects of re-entry flows [[electronic resource] /] / edited by James N. Moss, Carl D. Scott
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
Opac: Controlla la disponibilità qui
Thermophysical aspects of re-entry flows [[electronic resource] /] / edited by James N. Moss, Carl D. Scott
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
Opac: Controlla la disponibilità qui
Thermophysical aspects of re-entry flows [[electronic resource] /] / edited by James N. Moss, Carl D. Scott
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
Opac: Controlla la disponibilità qui