Comparison of flight pressure measurements with wind-tunnel data and theory for the forward fuselage of the X-15 airplane at Mach numbers from 0.8 to 6.0 /
Jon S. Pyle.

APA Citation

Pyle, J. S., Flight Research Center (U.S.)., United States. National Aeronautics and Space Administration. (1964). Comparison of flight pressure measurements with wind-tunnel data and theory for the forward fuselage of the X-15 airplane at Mach numbers from 0.8 to 6.0. Washington, D.C.: National Aeronautics and Space Administration .

MLA Citation

Pyle, Jon S, Flight Research Center (U.S.), and United States. National Aeronautics and Space Administration. Comparison of Flight Pressure Measurements With Wind-tunnel Data And Theory for the Forward Fuselage of the X-15 Airplane At Mach Numbers From 0.8 to 6.0. Washington, D.C.: National Aeronautics and Space Administration , 1964.