The effect of lateral area on the lateral stability and control characteristics of an airplane as determined by tests of a model in the Langley free-flight tunnel
Wartime report ; L-103
1946
13 S., [8] Bl
Ill., graph. Darst
Originally issued February 1946 as Advance restricted report L5L05
Report
Englisch
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
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