Supersedes NACA Tech Note n 2278, indexed in Engineering Index 1951 p 45.
Theoretical symmetric span loading due to flap deflection for wings of arbitrary plan form at subsonic speeds
NACA -- Report
1952
41 pages
Report
Englisch
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Engineering Index Backfile | 1951
|Theoretical symmetric span loading at subsonic speeds for wings having arbitrary plan form
Engineering Index Backfile | 1948
|