Thermophysical Aspects of Re-Entry Flows
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Published By American Institute Of Aeronautics And Astronautics

9780930403102, 9781600865770

Latest Documents Most Cited Documents Contributed Authors Related Sources Related Keywords

Thermophysical Aspects of Re-Entry Flows ◽

10.2514/5.9781600865770.0000.0000 ◽

1986 ◽

pp. i-xv

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Electron-Nitrogen Molecule Collisions in High-Temperature Nonequilibrium Air

Thermophysical Aspects of Re-Entry Flows ◽

10.2514/5.9781600865770.0152.0196 ◽

1986 ◽

pp. 152-196

Keyword(s):

High Temperature ◽

Nitrogen Molecule ◽

Temperature Nonequilibrium

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Author Index

Thermophysical Aspects of Re-Entry Flows ◽

10.2514/5.9781600865770.0620.0620 ◽

1986 ◽

pp. 620-620

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Drag of Bodies in Rarefied Hypersonic Flow

Thermophysical Aspects of Re-Entry Flows ◽

10.2514/5.9781600865770.0044.0059 ◽

1986 ◽

pp. 44-59 ◽

Cited By ~ 2

Keyword(s):

Hypersonic Flow

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Two Dimensional and Axisymmetric Heat-Transfer Results with the CSCM-S Upwind Implicit Algorithm

Thermophysical Aspects of Re-Entry Flows ◽

10.2514/5.9781600865770.0596.0619 ◽

1986 ◽

pp. 596-619 ◽

Cited By ~ 3

Keyword(s):

Heat Transfer ◽

Two Dimensional ◽

Implicit Algorithm

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Chemical and Thermal Nonequilibrium Heat-Transfer Analysis for Hypervelocity, Low Reynolds Number Flow

Thermophysical Aspects of Re-Entry Flows ◽

10.2514/5.9781600865770.0445.0477 ◽

1986 ◽

pp. 445-477

Keyword(s):

Heat Transfer ◽

Reynolds Number ◽

Low Reynolds Number ◽

Heat Transfer Analysis ◽

Thermal Nonequilibrium ◽

Low Reynolds Number Flow ◽

Reynolds Number Flow ◽

Number Flow ◽

Low Reynolds

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Developments in Aerothermal Test Techniques athe AEDC Supersonic/Hypersonic Wind Tunnels

Thermophysical Aspects of Re-Entry Flows ◽

10.2514/5.9781600865770.0373.0392 ◽

1986 ◽

pp. 373-392

Keyword(s):

Wind Tunnels

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Direct Simulation Monte Carlo Method and Comparison with Experiment

Thermophysical Aspects of Re-Entry Flows ◽

10.2514/5.9781600865770.0025.0043 ◽

1986 ◽

pp. 25-43 ◽

Cited By ~ 2

Keyword(s):

Monte Carlo ◽

Monte Carlo Method ◽

Direct Simulation Monte Carlo ◽

Direct Simulation ◽

Comparison With Experiment ◽

Simulation Monte Carlo

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Three-Dimensional Viscous Shock Layer Applications for the Space Shuttle Orhiter

Thermophysical Aspects of Re-Entry Flows ◽

10.2514/5.9781600865770.0541.0570 ◽

1986 ◽

pp. 541-570

Keyword(s):

Shock Layer ◽

Space Shuttle ◽

Three Dimensional ◽

Viscous Shock Layer

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Effects of Surface Discontinuities on Convective Heat Transfer in Hypersonic Flow

Thermophysical Aspects of Re-Entry Flows ◽

10.2514/5.9781600865770.0416.0442 ◽

1986 ◽

pp. 416-442

Keyword(s):

Heat Transfer ◽

Convective Heat Transfer ◽

Hypersonic Flow ◽

Convective Heat ◽

Surface Discontinuities

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Thermophysical Aspects of Re-Entry Flows
Latest Publications

TOTAL DOCUMENTS

H-INDEX

Published By American Institute Of Aeronautics And Astronautics

Table of Contents

Electron-Nitrogen Molecule Collisions in High-Temperature Nonequilibrium Air

Author Index

Drag of Bodies in Rarefied Hypersonic Flow

Two Dimensional and Axisymmetric Heat-Transfer Results with the CSCM-S Upwind Implicit Algorithm

Chemical and Thermal Nonequilibrium Heat-Transfer Analysis for Hypervelocity, Low Reynolds Number Flow

Developments in Aerothermal Test Techniques athe AEDC Supersonic/Hypersonic Wind Tunnels

Direct Simulation Monte Carlo Method and Comparison with Experiment

Three-Dimensional Viscous Shock Layer Applications for the Space Shuttle Orhiter

Effects of Surface Discontinuities on Convective Heat Transfer in Hypersonic Flow

Export Citation Format

Thermophysical Aspects of Re-Entry FlowsLatest Publications

TOTAL DOCUMENTS

H-INDEX

Published By American Institute Of Aeronautics And Astronautics

Table of Contents

Electron-Nitrogen Molecule Collisions in High-Temperature Nonequilibrium Air

Author Index

Drag of Bodies in Rarefied Hypersonic Flow

Two Dimensional and Axisymmetric Heat-Transfer Results with the CSCM-S Upwind Implicit Algorithm

Chemical and Thermal Nonequilibrium Heat-Transfer Analysis for Hypervelocity, Low Reynolds Number Flow

Developments in Aerothermal Test Techniques athe AEDC Supersonic/Hypersonic Wind Tunnels

Direct Simulation Monte Carlo Method and Comparison with Experiment

Three-Dimensional Viscous Shock Layer Applications for the Space Shuttle Orhiter

Effects of Surface Discontinuities on Convective Heat Transfer in Hypersonic Flow

Thermophysical Aspects of Re-Entry Flows
Latest Publications