Low scale wing tunnel investigation conducted in both straight and yawing flow; curved flow equipment of Langley stability tunnel used for tests.
Investigation at low speeds of effect of aspect ratio and sweep on static and yawing stability derivatives of untapered wings
Nat Advisory Committee Aeronautics -- Tech Note
1948
34 pages
Bibliography
Aufsatz (Zeitschrift)
Englisch
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Engineering Index Backfile | 1950
|Engineering Index Backfile | 1949
|Downwash and wake behind untapered wings of various aspect ratios and angles of sweep
Engineering Index Backfile | 1948
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