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Static Stability and Separation Characteristics of a Two-stage Rocket Configuration at Mach Numbers from 1.57 to 4.50: Volume 188
Kenneth L. Turner
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David S. Shaw
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Laurence William Enderson
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¡ National Aeronautics and Space Administration
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Wind-tunnel Investigation of Static Aerodynamic Characteristics of a 1/9-scale Model of a Project Mercury Capsule at Mach Numbers from 1.60 to 4.65
David S. Shaw
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Wind-tunnel Investigation of Static Aerodynamic Characteristics of a 1/9-scale Model of a Project Mercury Capsule at Mach Numbers from 1.60 to 4.65
David S. Shaw
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Wind-tunnel Investigation of Static Aerodynamic Characteristics of a 1/9-scale Model of a Possible Reentry Capsule at Mach Numbers from 2.29 to 4.65
David S. Shaw
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Effects of Nose Bluntness, Fineness Ratio, Cone Angle, and Model Base on the Static Aerodynamic Characteristics of Blunt Bodies at Mach Numbers of 1.57, 1.80, and 2.16 and Angles of Attack Up to 180 Ė
David S. Shaw
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Effect of Cross-section Shape on the Aerodynamics Characteristics of Bodies at Mach Numbers from 2.50 to 4.63
Dennis E. Fuller
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