NASA technical note TN (series). D-3447. Measured and calculated flow conditions on forward fuselage of X-15 airplane and model at Mach numbers from 3.0 to 8.0 [with list of references]; by Murray Palitz.
Publication Title:
Measured and calculated flow conditions on forward fuselage of X-15 airplane and model at Mach numbers from 3.0 to 8.0 [with list of references]; by Murray Palitz.
Display Title:
NASA technical note TN (series). D-3447. Measured and calculated flow conditions on forward fuselage of X-15 airplane and model at Mach numbers from 3.0 to 8.0 [with list of references]; by Murray Palitz.