Longitudinal and Lateral Stability and Control Characteristics at Mach Number 2.01 of a 60 Degree Delta-wing Airplane Configuration Equipped with a Canard Control and with Wing Trailing-edge Flap Controls

Longitudinal and Lateral Stability and Control Characteristics at Mach Number 2.01 of a 60 Degree Delta-wing Airplane Configuration Equipped with a Canard Control and with Wing Trailing-edge Flap Controls PDF Author: M. Leroy Spearman
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ISBN:
Category :
Languages : en
Pages : 51

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Effects of Wing Height on the Stability and Control Characteristics at a Mach Number of 2.01 of a Canard Airplane Configuration with a 70 Deg Delta Wing

Effects of Wing Height on the Stability and Control Characteristics at a Mach Number of 2.01 of a Canard Airplane Configuration with a 70 Deg Delta Wing PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 36

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Longitudinal Stability and Control Characteristics at Mach Numbers from 0.70 to 2.22 of a Triangular Wing Configuration Equipped with a Canard Control, a Trailing-edge-flap Control, Or a Cambered Forebody

Longitudinal Stability and Control Characteristics at Mach Numbers from 0.70 to 2.22 of a Triangular Wing Configuration Equipped with a Canard Control, a Trailing-edge-flap Control, Or a Cambered Forebody PDF Author: John W. Boyd
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ISBN:
Category :
Languages : en
Pages : 36

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Longitudinal Stability and Control Characteristics at Mach Numbers from 0.70 to 2.22 of Triangular Wing Configuration Equipped with Canard Control, Trailing-edge Flap Control, Or Cambered Forebody [with List of References]

Longitudinal Stability and Control Characteristics at Mach Numbers from 0.70 to 2.22 of Triangular Wing Configuration Equipped with Canard Control, Trailing-edge Flap Control, Or Cambered Forebody [with List of References] PDF Author:
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ISBN:
Category :
Languages : en
Pages : 39

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Low-speed Static Longitudinal and Lateral Stability Characteristics of a Variable-incidence Delta-wing Canard Model with High-lift Canard Surfaces

Low-speed Static Longitudinal and Lateral Stability Characteristics of a Variable-incidence Delta-wing Canard Model with High-lift Canard Surfaces PDF Author: Clarence D. Cone (Jr.)
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ISBN:
Category : Airplanes
Languages : en
Pages : 76

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Effect of Longitudinal and Lateral Controls on Winged Reentry Configuration at Mach 1.97 and Angles of Attack Up to 90°

Effect of Longitudinal and Lateral Controls on Winged Reentry Configuration at Mach 1.97 and Angles of Attack Up to 90° PDF Author: Gerald V. Foster
Publisher:
ISBN:
Category : Angle of attack (Aerodynamics)
Languages : en
Pages : 20

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Static Longitudinal, Directional, and Lateral Stability and Control Data at a Mach Number of 6.83 of the Final Configuration of the X-15 Research Airplane

Static Longitudinal, Directional, and Lateral Stability and Control Data at a Mach Number of 6.83 of the Final Configuration of the X-15 Research Airplane PDF Author: Jim A. Penland
Publisher:
ISBN:
Category : Aerodynamic measurements
Languages : en
Pages : 150

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Low-speed Static Lateral Stability Characteristics of a Canard Model Having a 60© Triangular Wing and Horizontal Tail

Low-speed Static Lateral Stability Characteristics of a Canard Model Having a 60© Triangular Wing and Horizontal Tail PDF Author: William R. Bates
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ISBN:
Category : Airplanes
Languages : en
Pages : 38

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Span Loadings and Aerodynamic Characteristics for a Series of Tip and Trailing-edge Controls on a 60° Delta Wing at Mach Numbers of 1.61 and 2.01

Span Loadings and Aerodynamic Characteristics for a Series of Tip and Trailing-edge Controls on a 60° Delta Wing at Mach Numbers of 1.61 and 2.01 PDF Author: K. R. Czarnecki
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 124

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Longitudinal Stability and Control Characteristics at Mach Numbers of 1.41 and 2.01 of a 67 Degree Swept-wing Airplane Configuration with Canard Control Surfaces

Longitudinal Stability and Control Characteristics at Mach Numbers of 1.41 and 2.01 of a 67 Degree Swept-wing Airplane Configuration with Canard Control Surfaces PDF Author: M. Leroy Spearman
Publisher:
ISBN:
Category :
Languages : en
Pages : 36

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