Theoretical symmetric span loading due to flap deflection for wings of arbitrary plan form at subsonic speeds.
Theoretical symmetric span loading due to flap deflection for wings of arbitrary plan form at subsonic speeds
Nat Advisory Committee Aeronautics -- Tech Note
1951
71 pages
Charts, Tables
Report
Englisch
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Engineering Index Backfile | 1952
|Theoretical symmetric span loading at subsonic speeds for wings having arbitrary plan form
Engineering Index Backfile | 1948
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