Aerodynamic Characteristics in Pitch at a Mach Number of 1.97 of Two Variable-wing- Sweep V/STOL Configurations with Outboard Wing Panels Swept Back 75 Deg

Aerodynamic Characteristics in Pitch at a Mach Number of 1.97 of Two Variable-wing- Sweep V/STOL Configurations with Outboard Wing Panels Swept Back 75 Deg PDF Author:
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ISBN:
Category :
Languages : en
Pages : 28

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Aerodynamic Characteristics in Pitch at a Mach Number of 1.97 of Two Variable-wing- Sweep V/STOL Configurations with Outboard Wing Panels Swept Back 75°

Aerodynamic Characteristics in Pitch at a Mach Number of 1.97 of Two Variable-wing- Sweep V/STOL Configurations with Outboard Wing Panels Swept Back 75° PDF Author: Gerald V. Foster
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ISBN:
Category : Airplanes
Languages : en
Pages : 22

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Static Longitudinal and Lateral Aerodynamic Characteristics at a Mach Number of 2.20 of a V/STOL Airplane Configuration with a Variable-sweep Wing and with a Skewed Wing Design

Static Longitudinal and Lateral Aerodynamic Characteristics at a Mach Number of 2.20 of a V/STOL Airplane Configuration with a Variable-sweep Wing and with a Skewed Wing Design PDF Author: Odell A. Morris
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ISBN:
Category : Airplanes
Languages : en
Pages : 32

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Stability and Control Characteristics at a Mach Number of 2.01 of a Variable-wing-sweep Configuration with Outboard Wing Panels Swept Back 75 Deg

Stability and Control Characteristics at a Mach Number of 2.01 of a Variable-wing-sweep Configuration with Outboard Wing Panels Swept Back 75 Deg PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 22

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Static Longitudinal and Lateral Aerodynamic Characteristics at a Mach Number of 2.20 of a V/STOL Airplane Configuration with a Variable-sweep Wing and with a Skewed Wing Design

Static Longitudinal and Lateral Aerodynamic Characteristics at a Mach Number of 2.20 of a V/STOL Airplane Configuration with a Variable-sweep Wing and with a Skewed Wing Design PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 32

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Stability and Control Characteristics at Mach Numbers of 2.50, 3.00, and 3.71 of a Variable- Wing-sweep Configuration with Outboard Wing Panels Swept Back 75 Deg

Stability and Control Characteristics at Mach Numbers of 2.50, 3.00, and 3.71 of a Variable- Wing-sweep Configuration with Outboard Wing Panels Swept Back 75 Deg PDF Author:
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Category :
Languages : en
Pages : 38

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Aerodynamic Characteristics at a Mach Number of 2.20 of a Variable-sweep Fighter Model with Wing Sweep of 50 Deg, 60 Deg, and 75 Deg

Aerodynamic Characteristics at a Mach Number of 2.20 of a Variable-sweep Fighter Model with Wing Sweep of 50 Deg, 60 Deg, and 75 Deg PDF Author:
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ISBN:
Category :
Languages : en
Pages : 38

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Static Longitudinal and Lateral Aerodynamic Characteristics at a Mach Number of 2.01 of a Tailless Delta V/STOL Configuration Having Variable-sweep Wing Panels

Static Longitudinal and Lateral Aerodynamic Characteristics at a Mach Number of 2.01 of a Tailless Delta V/STOL Configuration Having Variable-sweep Wing Panels PDF Author: M. Leroy Spearman
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ISBN:
Category : Airplanes
Languages : en
Pages : 36

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Longitudinal Aerodynamic Characteristics at Transonic Speeds of Two V/STOL Airplane Configurations with Skewed and Variable-sweep Wings

Longitudinal Aerodynamic Characteristics at Transonic Speeds of Two V/STOL Airplane Configurations with Skewed and Variable-sweep Wings PDF Author:
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ISBN:
Category :
Languages : en
Pages : 104

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Static Longitudinal and Lateral Aerodynamic Characteristics at a Mach Number of 2.01 of a Tailless Delta V/STOL Configuration Having Variable-sweep Wing Panels

Static Longitudinal and Lateral Aerodynamic Characteristics at a Mach Number of 2.01 of a Tailless Delta V/STOL Configuration Having Variable-sweep Wing Panels PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 36

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