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NASA Technical Note [D-135] : FULL-SCALE WIND-TUNNEL TESTS OF A LOW-ASPECTS-RATIO, STRAIGHT-WING AIRPLANE WITH BLOWING BOUNDARY-LAYER CONTROL ON LEADING-AND TRAILING-EDGE FLAPS

By: Contributor(s): Series: National Aeronautics and Space Administration (NASA) | NASA Technical NotePublication details: NASA, Washington, D.C. 1959Description: 37pSubject(s):
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NASA Technical Notes D-131-140
Bounded Volumes Accession No. 63638; Contents: TR16036-44

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