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)