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|a TL1060
|b .T44 1986eb
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0 |
4 |
|a 629.1 s
|a 629.4/152
|2 19
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| 049 |
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|a UAMI
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| 245 |
0 |
0 |
|a Thermophysical aspects of re-entry flows /
|c edited by James N. Moss, Carl D. Scott.
|
| 260 |
|
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|a New York, N.Y. :
|b American Institute of Aeronautics and Astronautics,
|c ©1986.
|
| 300 |
|
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|a 1 online resource (xv, 620 pages) :
|b illustrations
|
| 336 |
|
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|a text
|b txt
|2 rdacontent
|
| 337 |
|
|
|a computer
|b c
|2 rdamedia
|
| 338 |
|
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|a online resource
|b cr
|2 rdacarrier
|
| 490 |
1 |
|
|a Progress in astronautics and aeronautics ;
|v v. 103
|
| 500 |
|
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|a "Technical papers selected from the AIAA 23rd Aerospace Sciences Meeting, January 1985, and the AIAA 20th Thermophysics Conference, June 1985, and subsequently revised."
|
| 504 |
|
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|a Includes bibliographical references and index.
|
| 505 |
0 |
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|a 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
|
| 505 |
8 |
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|a 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
|
| 505 |
8 |
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|a 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
|
| 505 |
8 |
|
|a 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
|
| 590 |
|
|
|a ProQuest Ebook Central
|b Ebook Central Academic Complete
|
| 650 |
|
0 |
|a Space vehicles
|x Atmospheric entry.
|
| 650 |
|
0 |
|a Aerothermodynamics.
|
| 650 |
|
0 |
|a Aerodynamics, Hypersonic.
|
| 650 |
|
6 |
|a Véhicules spatiaux
|x Entrée dans l'atmosphère.
|
| 650 |
|
6 |
|a Aérothermodynamique.
|
| 650 |
|
6 |
|a Aérodynamique hypersonique.
|
| 650 |
|
7 |
|a Aerodynamics, Hypersonic
|2 fast
|
| 650 |
|
7 |
|a Aerothermodynamics
|2 fast
|
| 650 |
|
7 |
|a Space vehicles
|x Atmospheric entry
|2 fast
|
| 700 |
1 |
|
|a Moss, James N.
|
| 700 |
1 |
|
|a Scott, Carl D.
|
| 710 |
2 |
|
|a American Institute of Aeronautics and Astronautics.
|
| 711 |
2 |
|
|a AIAA Aerospace Sciences Meeting
|n (23rd :
|d 1985 :
|c Reno, Nev.)
|
| 711 |
2 |
|
|a AIAA Thermophysics Conference
|n (20th :
|d 1985 :
|c Williamsburg, Va.)
|
| 758 |
|
|
|i has work:
|a Thermophysical aspects of re-entry flows (Text)
|1 https://id.oclc.org/worldcat/entity/E39PD3hG7KkRBQ9rxdqxttMvPj
|4 https://id.oclc.org/worldcat/ontology/hasWork
|
| 776 |
0 |
8 |
|i Print version:
|t Thermophysical aspects of re-entry flows.
|d New York, N.Y. : American Institute of Aeronautics and Astronautics, ©1986
|w (DLC) 86010807
|
| 830 |
|
0 |
|a Progress in astronautics and aeronautics ;
|v v. 103.
|
| 856 |
4 |
0 |
|u https://ebookcentral.uam.elogim.com/lib/uam-ebooks/detail.action?docID=3111633
|z Texto completo
|
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