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Division of Load Among the Wing, Fuselage, and Tail of Aircraft
Report discussing the division of load among the wing, fuselage, and tail for several aircraft configurations at subsonic and supersonic speeds. The load that each component carries at various Mach numbers and angles of attack is described.
Date:
May 29, 1951
Creator:
Mayer, John P. & Gillis, Clarence L.
System:
The UNT Digital Library