NASA technical note TN (series). D-2241. Comparison of flight pressure measurements with wind-tunnel data and theory for forward fuselage of X-15 airplane at Mach numbers from 0.8 to 6.0 [with list of references]; by Jon S. Pyle.
Publication Title:
Comparison of flight pressure measurements with wind-tunnel data and theory for forward fuselage of X-15 airplane at Mach numbers from 0.8 to 6.0 [with list of references]; by Jon S. Pyle.
Display Title:
NASA technical note TN (series). D-2241. Comparison of flight pressure measurements with wind-tunnel data and theory for forward fuselage of X-15 airplane at Mach numbers from 0.8 to 6.0 [with list of references]; by Jon S. Pyle.