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 Download

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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 : 74

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Book Description

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 : 74

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Book Description

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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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 Characterictics of a Possible Reentry Capsule

Wind Tunnel Investigation at Mach Numbers from 0.20 to 1.17 of the Static Aerodynamic Characterictics of a Possible Reentry Capsule PDF Author: Albin O. Pearson
Publisher:
ISBN:
Category :
Languages : en
Pages : 26

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Wind-tunnel Investigation at Mach Numbers from 1.60 to 4.50 of the Static-stability Characteristics of Two Nonlifting Vehicles Suitable for Reentry

Wind-tunnel Investigation at Mach Numbers from 1.60 to 4.50 of the Static-stability Characteristics of Two Nonlifting Vehicles Suitable for Reentry PDF Author: Kenneth L. Turner
Publisher:
ISBN:
Category :
Languages : en
Pages : 34

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Investigation of Aerodynamic Effects of External Combustion Below Flat-plate Model in 10- by 10-foot Wind Tunnel at Mach 2.4

Investigation of Aerodynamic Effects of External Combustion Below Flat-plate Model in 10- by 10-foot Wind Tunnel at Mach 2.4 PDF Author: Robert G. Dorsch
Publisher:
ISBN:
Category : Mach number
Languages : en
Pages : 30

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Wind-tunnel Investigation at a Mach Number of 2.91 of Stability and Control Characteristics of Three Lifting Reentry Configurations at Angles of Attack Up to 90 Degrees

Wind-tunnel Investigation at a Mach Number of 2.91 of Stability and Control Characteristics of Three Lifting Reentry Configurations at Angles of Attack Up to 90 Degrees PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 42

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Wind Tunnel Measurements of Hysteresis in the Static Aerodynamic Characteristics of Aircraft

Wind Tunnel Measurements of Hysteresis in the Static Aerodynamic Characteristics of Aircraft PDF Author: J. F. Herman
Publisher:
ISBN:
Category : Hysteresis
Languages : en
Pages : 112

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Wind Tunnel Tests of Rectangular Finned Variable Gap Tangent Ogive-cylinder Model at Mach Numbers 1.75 to 4.50

Wind Tunnel Tests of Rectangular Finned Variable Gap Tangent Ogive-cylinder Model at Mach Numbers 1.75 to 4.50 PDF Author: Neil Arthur Zarin
Publisher:
ISBN:
Category : Rockets (Aeronautics)
Languages : en
Pages : 106

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Aerodynamic Characteristics of the 40- by 80/80- by 120-foot Wind Tunnel at NASA Ames Research Center

Aerodynamic Characteristics of the 40- by 80/80- by 120-foot Wind Tunnel at NASA Ames Research Center PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 30

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