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CFD Simulations of Boundary Layer Transition Flight Experiment Catalytic Coating DataA CFD analysis is performed to model the catalytic jump in surface heating rates measured as part of the Space Shuttle Boundary Layer Transition (BLT) flight experiment.
Document ID
20140004906
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Palmer, Grant E. (Engineering Research and Consulting, Inc. Mountain View, CA, United States)
Campbell, Charles H. (NASA Johnson Space Center Houston, TX United States)
Berger, Karen T. (NASA Ames Research Center Moffett Field, CA United States)
Date Acquired
May 6, 2014
Publication Date
June 24, 2013
Subject Category
Fluid Mechanics And Thermodynamics
Composite Materials
Report/Patent Number
ARC-E-DAA-TN6731
Meeting Information
Meeting: American Inst. of Aeronautics and Astronautics Thermophysics Conference
Location: San Diego, CA
Country: United States
Start Date: June 24, 2013
End Date: June 27, 2013
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NNA10DE12C
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
TPS
CFD
catalytic wall
Catalytic jump phenomena
Earth entry

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