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 Download

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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:
Publisher:
ISBN:
Category :
Languages : en
Pages : 34

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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:
Publisher:
ISBN:
Category :
Languages : en
Pages : 34

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Book Description

Transonic Wind Tunnel Investigation of the Static Longitudinal Aerodynamic Characteristics of Five Nose Cones Designed for Supersonic Impact

Transonic Wind Tunnel Investigation of the Static Longitudinal Aerodynamic Characteristics of Five Nose Cones Designed for Supersonic Impact PDF Author: John P. Jr Mugler
Publisher:
ISBN:
Category :
Languages : en
Pages : 30

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An Investigation at Mach Numbers from 1.47 to 2.87 of Static Stability Characteristics of Nine Nose Cones Designed for Supersonic Impact Velocities

An Investigation at Mach Numbers from 1.47 to 2.87 of Static Stability Characteristics of Nine Nose Cones Designed for Supersonic Impact Velocities PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 46

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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
Publisher:
ISBN:
Category : Hypersonic wind tunnels
Languages : en
Pages : 26

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Wind Tunnel Tests of the Redstone "B" Nose Cone at Mach Numbers from 1.75 to 5.00

Wind Tunnel Tests of the Redstone Author: Maurice A. Sylvester
Publisher:
ISBN:
Category : Launch vehicles (Astronautics)
Languages : en
Pages : 44

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Wind-tunnel Investigation at Mach Numbers from 0.40 to 1.14 of the Static Aerodynamic Characteristics of a Nonlifting Vehicle Suitable for Reentry

Wind-tunnel Investigation at Mach Numbers from 0.40 to 1.14 of the Static Aerodynamic Characteristics of a Nonlifting Vehicle Suitable for Reentry PDF Author: Albin O. Pearson
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 14

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Wind-tunnel Investigation at Mach Numbers from 0.20 to 1.17 of the Static Aerodynamic Characteristics of a Possible Reentry Capsule

Wind-tunnel Investigation at Mach Numbers from 0.20 to 1.17 of the Static Aerodynamic Characteristics of a Possible Reentry Capsule PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 30

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An Investigation at Mach Numbers from 0.20 to 4.63 of the Aerodynamic Performance, Static Stability, and Trimming Characteristics of a Canard Configuration Designed for Efficient Supersonic Cruise Flight

An Investigation at Mach Numbers from 0.20 to 4.63 of the Aerodynamic Performance, Static Stability, and Trimming Characteristics of a Canard Configuration Designed for Efficient Supersonic Cruise Flight PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 88

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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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Book Description

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:
Publisher:
ISBN:
Category :
Languages : en
Pages : 24

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Book Description