The Effects of Sideslip, Aspect Ratio, and Mach Number on the Lift and Pitching Moment of Triangular, Trapezoidal, and Related Plan Forms in Supersonic Flow
Language: en
Pages: 78

The Effects of Sideslip, Aspect Ratio, and Mach Number on the Lift and Pitching Moment of Triangular, Trapezoidal, and Related Plan Forms in Supersonic Flow

Authors: Arthur L. Jones
Categories: Aerofoils
Type: BOOK - Published: 1949 - Publisher:

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The variations of lift and pitching moment with sideslip in supersonic flow have been calculated for a representative gorup of plan forms. The variations of lif
Sideslip Characteristics at Various Angles of Attack for Several Hypersonic Missile Configurations with Canard Controls at a Mach Number of 2.01
Language: en
Pages: 30

Sideslip Characteristics at Various Angles of Attack for Several Hypersonic Missile Configurations with Canard Controls at a Mach Number of 2.01

Authors: Gerald V. Foster
Categories: Aerodynamics, Supersonic
Type: BOOK - Published: 1959 - Publisher:

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Aerodynamic Loading Characteristics in Sideslip of a 45© Sweptback Wing with and Without a Fence at High Subsonic Speeds
Language: en
Pages: 50

Aerodynamic Loading Characteristics in Sideslip of a 45© Sweptback Wing with and Without a Fence at High Subsonic Speeds

Authors: Richard E. Kuhn
Categories: Aerodynamic load
Type: BOOK - Published: 1955 - Publisher:

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Effect of Forebody Strakes on the Aerodynamic Characteristics in Pitch and Sideslip of a Hypersonic Airplane Configuration at Mach Numbers of 1.41, 2.01, and 6.86
Language: en
Pages: 56

Effect of Forebody Strakes on the Aerodynamic Characteristics in Pitch and Sideslip of a Hypersonic Airplane Configuration at Mach Numbers of 1.41, 2.01, and 6.86

Authors: Cornelius Driver
Categories: Aerodynamic measurements
Type: BOOK - Published: 1959 - Publisher:

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The Yawing Moment Due to Sideslip of Triangular, Trapezoidal, and Related Plan Forms in Supersonic Flow
Language: en
Pages: 72

The Yawing Moment Due to Sideslip of Triangular, Trapezoidal, and Related Plan Forms in Supersonic Flow

Authors: Arthur Leslie Jones
Categories: Aerodynamics, Supersonic
Type: BOOK - Published: 1949 - Publisher:

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The variation of the yawing moment with sideslip and the variation of the stability derivative with aspect ratio and Mach number were investigated.