Static Stability And Drag Characteristics Of A Hypersonic Aircraft Design At Mach Numbers 15 To 56
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Static Stability and Drag Characteristics of a Hypersonic Aircraft Design at Mach Numbers 1.5 to 5.6
| Author | : J. T. Best (Jr.) |
| Publisher | : |
| Total Pages | : 122 |
| Release | : 1975 |
| Genre | : Drag (Aerodynamics) |
| ISBN | : |
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Type: BOOK - Published: 1975 - Publisher:
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Type: BOOK - Published: 1968 - Publisher:
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Aerodynamic characteristics of a model designed to represent an all body, hypersonic cruise aircraft are presented for Mach numbers from 0.65 to 10.6. The confi
Language: en
Pages: 42
Pages: 42
Type: BOOK - Published: 1960 - Publisher:
An aircraft configuration, previously conceived as a means to achieve favorable aerodynamic stability characteristics., high lift-drag ratio, and low heating ra
