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001 EBC3111633
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006 m o d |
007 cr cnu||||||||
008 200713s1986 xx o ||||0 eng d
020 9781600863585|q(electronic bk.)
020 |z9780930403102
035 (MiAaPQ)EBC3111633
035 (Au-PeEL)EBL3111633
035 (CaPaEBR)ebr10516738
035 (OCoLC)922979052
040 MiAaPQ|beng|erda|epn|cMiAaPQ|dMiAaPQ
050 4 TL1060 -- .T44 1986eb
082 0 629.1 s;629.4/152
100 1 Scott, Carl D
245 10 Thermophysical Aspects of Re-Entry Flows
264 1 Reston :|bAmerican Institute of Aeronautics and
Astronautics,|c1986
264 4 |c©1986
300 1 online resource (636 pages)
336 text|btxt|2rdacontent
337 computer|bc|2rdamedia
338 online resource|bcr|2rdacarrier
490 1 Progress in Astronautics and Aeronautics ;|vv.103
505 0 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
505 8 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
588 Description based on publisher supplied metadata and other
sources
590 Electronic reproduction. Ann Arbor, Michigan : ProQuest
Ebook Central, 2020. Available via World Wide Web. Access
may be limited to ProQuest Ebook Central affiliated
libraries
650 0 Space vehicles -- Atmospheric
entry.;Aerothermodynamics.;Aerodynamics, Hypersonic
655 4 Electronic books
700 1 Moss, James N
776 08 |iPrint version:|aScott, Carl D.|tThermophysical Aspects
of Re-Entry Flows|dReston : American Institute of
Aeronautics and Astronautics,c1986|z9780930403102
830 0 Progress in Astronautics and Aeronautics
856 40 |uhttps://ebookcentral.proquest.com/lib/sinciatw/
detail.action?docID=3111633|zClick to View
