NASA technical note TN (series). D-2604. Aerodynamic load distributions for project fire configurations at Mach numbers from 0.25 to 4.63 [with list of references]; by Ralph J. Muraca.
Publication Title:
Aerodynamic load distributions for project fire configurations at Mach numbers from 0.25 to 4.63 [with list of references]; by Ralph J. Muraca.
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NASA technical note TN (series). D-2604. Aerodynamic load distributions for project fire configurations at Mach numbers from 0.25 to 4.63 [with list of references]; by Ralph J. Muraca.