Investigation of stability and control characteristics of an airplane model with skewed wing in the Langley free-flight tunnel
1947
13 S., Fig. 1 - 14
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
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Engineering Index Backfile | 1947
|Engineering Index Backfile | 1946
|Engineering Index Backfile | 1945
|Flight tests of airplane model with 62° swept-back wing in Langley free-flight tunnel
Engineering Index Backfile | 1947
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