Longitudinal Aerodynamic Characteristics at Mach Numbers from 0.50 to 1.19 of a Supersonic Transport Model with a Modified M Wing PDF Download

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Longitudinal Aerodynamic Characteristics at Mach Numbers from 0.50 to 1.19 of a Supersonic Transport Model with a Modified M Wing

Author: Edward J. Ray
Publisher:
ISBN:
Category :
Languages : en
Pages : 84

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Author: Edward J. Ray
Publisher:
ISBN:
Category :
Languages : en
Pages : 84

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Book Description

Low-speed Longitudinal Aerodynamic Characteristics of a Supersonic Transport Model Having a Variable-sweep M Wing PDF

Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 76

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Aerodynamic Characteristics at Mach Numbers 2.30, 2.60, and 2.96 of a Supersonic Transport Model Having a Fixed, Warped Wing PDF

Author:
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ISBN:
Category :
Languages : en
Pages : 68

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Book Description

Aerodynamic Characteristics of a Tailless Fixed-wing Supersonic Transport Configuration at Mach Number 2.20 PDF

Author: Gerald V. Foster
Publisher:
ISBN:
Category : Airplanes, Tailless
Languages : en
Pages : 54

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Transonic Aerodynamic Characteristics of a Tailless Fixed-wing Supersonic Transport Model PDF

Author: Edward J. Ray
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 84

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Book Description

Aerodynamic Characteristics at Mach Numbers from 0.50 to 2.96 of a Supersonic Transport Model with a Variable-sweep High-panel-aspect-ratio Wing PDF

Author:
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ISBN:
Category :
Languages : en
Pages : 94

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Book Description

Aerodynamic Characteristics of a Three-engine Supersonic Transport Model Having a Low-aspect-ratio Variable-sweep Warped Wing PDF

Author: Odell A. Morris
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 72

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Book Description

Longitudinal Aerodynamic Characteristics of a High-subsonic-speed Transport Airplane Model with a Cambered 40° Sweptback Wing of Aspect Ratio 8 at Mach Numbers to 0.96 PDF

Author: Atwood R. Heath
Publisher:
ISBN:
Category : Mach number
Languages : en
Pages : 92

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Book Description

Aerodynamic Characteristics at Mach Numbers from 2.30 to 4.63 of a Supersonic Transport Model with a Variable-sweep M Wing PDF

Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 100

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Book Description

Aerodynamic Characteristics at Mach 2.30, 2.60, and 2.96 of a Supersonic Transport Model with a Modified Wing PDF

Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 76

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Book Description