Static Aerodynamic Characteristics at Mach Numbers from 2.50 to 4.63 of a Staged Airplane Model Designed for Cruise Above Mach 5

Static Aerodynamic Characteristics at Mach Numbers from 2.50 to 4.63 of a Staged Airplane Model Designed for Cruise Above Mach 5
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Total Pages: 62
Release: 1964
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