Stability and Control Characteristics at a Mach Number of 1.97 of an Airplane Configuration Having Two Types of Variable- Sweep Wings

Stability and Control Characteristics at a Mach Number of 1.97 of an Airplane Configuration Having Two Types of Variable- Sweep Wings PDF Author:
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Category :
Languages : en
Pages : 48

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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°

Stability and Control Characteristics at a Mach Number of 2.01 of a Variable-wing-sweep Configuration with Outboard Wing Panels Swept Back 75° PDF Author: M. Leroy Spearman
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Category : Airplanes
Languages : en
Pages : 26

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Stability and Control Characteristics at Low Subsonic Speeds of an Airplane Configuration Having Two Types of Variable-sweep Wings

Stability and Control Characteristics at Low Subsonic Speeds of an Airplane Configuration Having Two Types of Variable-sweep Wings PDF Author:
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Category :
Languages : en
Pages : 94

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Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
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Category : Aeronautics
Languages : en
Pages : 1330

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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°

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° PDF Author: Gerald V. Foster
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Category : Aerodynamics, Supersonic
Languages : en
Pages : 38

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Stability and Control Characteristics at a Mach Number of 2.01 of a Variable-sweep Airplane Configuration Capable of Low-level Supersonic Attack - Outer Wing Swept 75 Deg

Stability and Control Characteristics at a Mach Number of 2.01 of a Variable-sweep Airplane Configuration Capable of Low-level Supersonic Attack - Outer Wing Swept 75 Deg PDF Author:
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ISBN:
Category :
Languages : en
Pages : 24

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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:
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Category :
Languages : en
Pages : 22

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Keywords Index to U.S. Government Technical Reports

Keywords Index to U.S. Government Technical Reports PDF Author: United States. Department of Commerce. Office of Technical Services
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Category : Government publications
Languages : en
Pages : 978

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Stability and Control Characteristics at a Mach Number of 1.41 of a Variable-sweep Airplane Configuration Capable of Low-level Supersonic Attack-outer Wing Swept 75 Deg and 108 Deg

Stability and Control Characteristics at a Mach Number of 1.41 of a Variable-sweep Airplane Configuration Capable of Low-level Supersonic Attack-outer Wing Swept 75 Deg and 108 Deg PDF Author:
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Languages : en
Pages : 28

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Stability and Control Characteristics at a Mach Number of 2.2 of a Variable-sweep Airplane Configuration Having a 12-percent-pivot Location

Stability and Control Characteristics at a Mach Number of 2.2 of a Variable-sweep Airplane Configuration Having a 12-percent-pivot Location PDF Author:
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Category :
Languages : en
Pages : 20

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