3 edition of Pressure distributions from subsonic tests of an advanced laminar-flow-control wing with leading- and trailing-edge flaps found in the catalog.
Pressure distributions from subsonic tests of an advanced laminar-flow-control wing with leading- and trailing-edge flaps
Zachary T. Applin
by National Aeronautics and Space Administration, Scientific and Technical Information Division, For sale by the National Technical Information Service] in [Washington, D.C.], [Springfield, Va
Written in English
|Statement||Zachary T. Applin and Garl L. Gentry, Jr.|
|Series||NASA technical memorandum -- 4040.|
|Contributions||Gentry, Garl L., United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.|
|The Physical Object|
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