design approach and selected wind-tunnel results at high subsonic speeds for wing-tip mounted winglets.
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design approach and selected wind-tunnel results at high subsonic speeds for wing-tip mounted winglets.

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Published by National Aeronautics and Space Administration in Washington, DC .
Written in English


Book details:

Edition Notes

SeriesTechnical notes / National Aeronautics and Space Administration -- TND-8260
ID Numbers
Open LibraryOL20137673M

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