3 edition of Effects of wing sweep on in-flight boundary-layer transition for a laminar flow wing at Mach numbers from 0.60 to 0.79 found in the catalog.
Effects of wing sweep on in-flight boundary-layer transition for a laminar flow wing at Mach numbers from 0.60 to 0.79
by National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, For sale by the National Technical Information Service in Edwards, Calif, [Springfield, Va
Written in English
|Statement||Bianca Trujillo Anderson and Robert R. Meyer, Jr.|
|Series||NASA technical memorandum -- 101701.|
|Contributions||Meyer, Robert R., Dryden Flight Research Facility.|
|The Physical Object|
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