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Boundary Layer Transition Flight Experiment Implementation on OV-103This slide presentation reviews the boundary layer transition experiment flown on Discovery. The purpose of the boundary layer transition flight experiment was to obtain hypersonic aero-thermodynamic data for the purpose of better understanding the flow transition from a laminar to turbulent boundary layer using a known height protuberance. The preparation of the shuttle is described, with the various groups responsibilities outlined. Views of the shuttle in flight with the experimental results are shown.
Document ID
20110008506
Acquisition Source
Kennedy Space Center
Document Type
Presentation
Authors
Spanos, Theodoros A.
(NASA Kennedy Space Center Cocoa Beach, FL, United States)
Date Acquired
August 25, 2013
Publication Date
December 10, 2009
Subject Category
Astrodynamics
Report/Patent Number
KSC-2009-304
Report Number: KSC-2009-304
Meeting Information
Meeting: Kennedy Engineering Academy
Location: Kennedy Space Center, FL
Country: United States
Start Date: December 10, 2009
Funding Number(s)
CONTRACT_GRANT: NNJ06VA01C
Distribution Limits
Public
Copyright
Public Use Permitted.
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