Indexed in Engineering Index 1938 p 30, from Tech Report n 634.
Calculation of chordwise load distribution over airfoil sections with plain, split, or serially hinged trailing-edged flaps
Nat Advisory Committee Aeronautics -- 24th Annual Report
1938
16 pages
Report
Englisch
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Engineering Index Backfile | 1938
|Engineering Index Backfile | 1938
|Pressure distribution over N.A.C.A. 23012 airfoil with slotted and plain flaps
Engineering Index Backfile | 1938
|