Experimental and theoretical aerodynamic characteristics of two hypersonic cruise aircraft concepts at Mach numbers of 2.96, 3.96, and 4.63 /
Jimmy L. Pittman and Gregory D. Riebe.

APA Citation

Pittman, J. L., Riebe, G. D., Langley Research Center., United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch. (1980). Experimental and theoretical aerodynamic characteristics of two hypersonic cruise aircraft concepts at Mach numbers of 2.96, 3.96, and 4.63. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch .

MLA Citation

Pittman, Jimmy L, Gregory D Riebe, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch. Experimental And Theoretical Aerodynamic Characteristics of Two Hypersonic Cruise Aircraft Concepts At Mach Numbers of 2.96, 3.96, And 4.63. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch , 1980.

Warning: These citations may not always be complete (especially for serials).