Pressure distributions from subsonic tests of an advanced laminar-flow-control wing with leading- and trailing-edge flaps
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Pressure distributions from subsonic tests of an advanced laminar-flow-control wing with leading- and trailing-edge flaps

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Published 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

Subjects:

  • Aerodynamics.

Book details:

Edition Notes

StatementZachary T. Applin and Garl L. Gentry, Jr.
SeriesNASA technical memorandum -- 4040.
ContributionsGentry, Garl L., United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.
The Physical Object
FormatMicroform
Pagination1 v.
ID Numbers
Open LibraryOL14663372M

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