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
1946-01-01
Sonstige
Keine Angabe
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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