Determination of stability and control characteristics of tailless all-wing airplane model with sweepback in Langley free-flight tunnel (Originally issued as Advance Confidential Report L5A12 Feb 1945)
Determination of stability and control characteristics of tailless all-wing airplane model with sweepback in Langley free-flight tunnel
Nat Advisory Committee Aeronautics -- Wartime Report
1945
16 pages
16 Supp plates
Report
Englisch
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Engineering Index Backfile | 1946
|Flight tests of airplane model with 62° swept-back wing in Langley free-flight tunnel
Engineering Index Backfile | 1947
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