A Wind Tunnel Investigation of the Aerodynamic Characteristics of Bodies of Revolution at Mach Numbers of 2.37, 2.98, and 3.90

A Wind Tunnel Investigation of the Aerodynamic Characteristics of Bodies of Revolution at Mach Numbers of 2.37, 2.98, and 3.90 PDF Author: Fred M. Smith
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ISBN:
Category :
Languages : en
Pages : 35

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A Wind-tunnel Investigation of the Aerodynamic Characteristics of Bodies of Revolution at Mach Numbers of 2.37, 2.98, and 3.90 at Angles of Attack to 90 Deg

A Wind-tunnel Investigation of the Aerodynamic Characteristics of Bodies of Revolution at Mach Numbers of 2.37, 2.98, and 3.90 at Angles of Attack to 90 Deg PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 40

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Wind-tunnel Investigation at Mach Numbers from 0.60 to 1.20 of the Static Aerodynamic Characteristics of a Model of a Possible Nonlifting Reentry Capsule in Combination with a Rocket Booster

Wind-tunnel Investigation at Mach Numbers from 0.60 to 1.20 of the Static Aerodynamic Characteristics of a Model of a Possible Nonlifting Reentry Capsule in Combination with a Rocket Booster PDF Author: Albin O. Pearson
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 22

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A Wind-tunnel Investigation of Effects of Noise Bluntness, Face Shape, and Afterbody Length on the Aerodynamic Characteristics of Bodies of Revolution at Mach Numbers of 2.37, 2.98, and 3.90

A Wind-tunnel Investigation of Effects of Noise Bluntness, Face Shape, and Afterbody Length on the Aerodynamic Characteristics of Bodies of Revolution at Mach Numbers of 2.37, 2.98, and 3.90 PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 48

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Wind-tunnel Investigation at Mach Numbers from 3.0 to 6.8 of the Static Aerodynamic Characteristics of Modified Mercury Exit and Escape Capsule Configurations

Wind-tunnel Investigation at Mach Numbers from 3.0 to 6.8 of the Static Aerodynamic Characteristics of Modified Mercury Exit and Escape Capsule Configurations PDF Author: Albin O. Pearson
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ISBN:
Category : Hypersonic wind tunnels
Languages : en
Pages : 26

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Wind-tunnel Investigation at Mach Numbers from 0.50 to 1.14 of the Static Aerodynamic Characteristics of a Model of a Project Mercury Capsule

Wind-tunnel Investigation at Mach Numbers from 0.50 to 1.14 of the Static Aerodynamic Characteristics of a Model of a Project Mercury Capsule PDF Author: Albin O. Pearson
Publisher:
ISBN:
Category : Space vehicles
Languages : en
Pages : 34

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Wind-tunnel Investigation at Mach Numbers from 0.40 to 1.20 of the Static Aerodynamic and Control Characteristics of a Model of a Nonlifting Reeintry Capsule in Combination with a Rocket Booster

Wind-tunnel Investigation at Mach Numbers from 0.40 to 1.20 of the Static Aerodynamic and Control Characteristics of a Model of a Nonlifting Reeintry Capsule in Combination with a Rocket Booster PDF Author: Albin O. Pearson
Publisher:
ISBN:
Category : Space vehicles
Languages : en
Pages : 72

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Wind-tunnel Investigation at Mach Numbers from 1.47 to 4.62 of Static Aerodynamic Characteristics of Twelve Nose Cones Designed for Supersonic Impact

Wind-tunnel Investigation at Mach Numbers from 1.47 to 4.62 of Static Aerodynamic Characteristics of Twelve Nose Cones Designed for Supersonic Impact PDF Author:
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ISBN:
Category :
Languages : en
Pages : 34

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Full-scale Wind-tunnel Investigation of the Longitudinal Aerodynamic Characteristics of the M2-F1 Lifting Body Flight Vehicle

Full-scale Wind-tunnel Investigation of the Longitudinal Aerodynamic Characteristics of the M2-F1 Lifting Body Flight Vehicle PDF Author: Kenneth W. Mort
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ISBN:
Category : Space vehicles
Languages : en
Pages : 18

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A Wind Tunnel Investigation of Effects of Nose Bluntness, Face Shape, and Afterbody Length on the Aerodynamic Characteristics of Bodies of Revolution at Mach Numbers of 2.37, 2.93, and 3.90

A Wind Tunnel Investigation of Effects of Nose Bluntness, Face Shape, and Afterbody Length on the Aerodynamic Characteristics of Bodies of Revolution at Mach Numbers of 2.37, 2.93, and 3.90 PDF Author: Fred L. Smith
Publisher:
ISBN:
Category :
Languages : en
Pages : 44

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