Determination of Stability and Control Characteristics of Straight-Wing, Tailless Fighter-Airplane Model in Langley Free-Flight Tunnel. (Advance Confidential Report L5K05)
Determination of stability and control characteristics of straight-wing, tailless fighter-airplane model in Langley free-flight tunnel
Nat Advisory Committee Aeronautics -- Wartime Report
1946
16 pages
16 Supp plates
Report
Englisch
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Engineering Index Backfile | 1945
|Flight tests of airplane model with 62° swept-back wing in Langley free-flight tunnel
Engineering Index Backfile | 1947
|