The contents include: 1) Organization of the Orbiter Entry Aeroheating Working Group; 2) Overview of the Principal RTF Aeroheating Tools Utilized for Tile Damage Assessment; 3) Description of the Integrated Tile Damage Assessment Team Analyses Process; 4) Space Shuttle Flight Support Process; and 5) JSC Applied Aerosciences and CFD Branch Applied Research Interests.
Orbiter Entry Aerothermodynamics Practical Engineering and Applied Research
Fluid Mechanics Seminar ; 2009 ; Stanford, CA, United States
2009-04-12
Sonstige
Keine Angabe
Englisch
Configuration Aerothermodynamics of Entry Vehicles
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