Aerodynamic Characteristics At A Mach Number Of 310 Of Several Fourth Stage Shapes Of The Scout Research Vehicle
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Aerodynamic Characteristics at a Mach Number of 3.10 of Several Fourth-stage Shapes of the Scout Research Vehicle
| Author | : Byron M. Jaquet |
| Publisher | : |
| Total Pages | : 22 |
| Release | : 1961 |
| Genre | : Aerodynamics, Supersonic |
| ISBN | : |
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Language: en
Pages: 22
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Type: BOOK - Published: 1961 - Publisher:
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Pages: 1
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A wind-tunnel investigation was made at a Mach number of 3.10 (Reynolds number per foot of 16.3 x 10 to the 6th power to 16.9 x 10 to the 6th power) to determin
Language: en
Pages: 52
Pages: 52
Type: BOOK - Published: 1963 - Publisher:
Language: en
Pages: 42
Pages: 42
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Language: en
Pages: 68
Pages: 68
Type: BOOK - Published: 1961 - Publisher:
Aerodynamic loads results have been obtained in the Langley 8-foot transonic pressure tunnel at Mach numbers from 0.80 to 1.20 for a 1/10-scale model of the upp
