Investigation of lifting effectiveness and flow requirements of blowing boundary layer control applied to trailing edge flaps and ailerons of aircraft, with sufficient blowing jet momentum to prevent flow separation on flap, lift increment increased for flap deflections up to 80°.
Large-scale wind-tunnel tests of airplane model with un-swept, aspect-ratio-10 wing, two propellers, and blowing flaps
NASA -- Memo
National Aeronautics and Space Administration -- Memorandums ; Memo n 12-3-58A
1958
47 pages
Report
Englisch
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Engineering Index Backfile | 1959
|Engineering Index Backfile | 1958
|