Effects of wing incidence on the longitudinal trim characteristics of a cambered 70° delta-wing configuration at mach numbers 3.0 to 5.0 /
by Warren F. Ahtye.
APA Citation
Ahtye, W. F., Ames Research Center. (1960). Effects of wing incidence on the longitudinal trim characteristics of a cambered 70° delta-wing configuration at mach numbers 3.0 to 5.0. Washington, D.C.: National Aeronautics and Space Administration.
MLA Citation
Ahtye, Warren F, and Ames Research Center. Effects of Wing Incidence On the Longitudinal Trim Characteristics of a Cambered 70° Delta-wing Configuration At Mach Numbers 3.0 to 5.0. Washington, D.C.: National Aeronautics and Space Administration, 1960.
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