Pittman, J. L., & Riebe, G. D. (1980). Experimental and theoretical aerodynamic characteristics of two hypersonic cruise aircraft concepts at Mach numbers of 2.96, 3.96, and 4.63. National Aeronautics and Space Administration, Scientific and Technical Information Branch.
Chicago Style (17th ed.) CitationPittman, Jimmy L., and Gregory D. Riebe. 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.
MLA (9th ed.) CitationPittman, Jimmy L., and Gregory D. Riebe. Experimental and Theoretical Aerodynamic Characteristics of Two Hypersonic Cruise Aircraft Concepts at Mach Numbers of 2.96, 3.96, and 4.63. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1980.