Investigation at transonic speeds of the loading over a 40 degree sweptback wing having an aspect ratio of 3, a taper ratio of 0.2 and NACA 65A004 airfoil sections / by Jack F. Runckel and Edwin E. Lee, Jr.
|Main Author:||Runckel, Jack F.|
Washington, D.C. : National Aeronautics and Space Administration : 
Stresses and loads.
Aerodynamics, aircraft; Aircraft; Stresses and loads.
93 p. :
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