Lift tests of a 0.1536c thick Douglas airfoil section of NACA 7-series type equipped with a lateral-control device for use with a full-span double-slotted flap on the C-74 airplane
Wartime report ; L-641
1945
9 S., [30] Bl
Ill., graph. Darst
Originally issued March 1945 as Memorandum report L5C24a
Report
Englisch
Engineering Index Backfile | 1947
|Engineering Index Backfile | 1942
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