Flight tests, force tests, and damping in roll tests were made on model with wing set at angles of skew from 0° to 60°; investigation was of exploratory nature and was intended to provide only preliminary and qualitative indication of whether such design could be flown.
Investigation of stability and control characteristics of airplane model with skewed wing in Langley freeflight tunnel
Nat Advisory Committee Aeronautics -- Tech Note
1947
13 pages
Supp Sheets
Report
Englisch
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Engineering Index Backfile | 1946
|Engineering Index Backfile | 1945
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