Effect of Lateral Area on Lateral Stability and Control Characteristics of Airplane as Determined by Tests of Model in Langley Free-Flight Tunnel. (Advance Restricted Report L5L05 Feb 1946)
Effect of lateral area on lateral stability and control characteristics of airplane as determined by tests of model in Langley free-flight tunnel
Nat Advisory Committee Aeronautics -- Wartime Report
1946
13 pages
8 Supp plates
Report
English
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Engineering Index Backfile | 1946
|Engineering Index Backfile | 1943
|Flight tests of airplane model with 62° swept-back wing in Langley free-flight tunnel
Engineering Index Backfile | 1947
|