Related Books

Aerodynamic Characteristics of a Spoiler-slot-deflector Control on a 45© Sweptback Wing at Mach Numbers of 1.61 and 2.01
Language: en
Pages: 52

Aerodynamic Characteristics of a Spoiler-slot-deflector Control on a 45© Sweptback Wing at Mach Numbers of 1.61 and 2.01

Authors: Douglas R. Lord
Categories: Aerodynamics
Type: BOOK - Published: 1957 - Publisher:

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An investigation has been made in the Langley 4- by 4-foot supersonic pressure tunnel at Mach numbers of 1.61 and 2.01 to determine the aerodynamic characterist
Aerodynamic Characteristics of a Spoiler-slot-deflector Control on a 45° Sweptback-wing-fuselage Model at High Subsonic Speeds
Language: en
Pages: 80

Aerodynamic Characteristics of a Spoiler-slot-deflector Control on a 45° Sweptback-wing-fuselage Model at High Subsonic Speeds

Authors: Alexander D. Hammond
Categories: Aerodynamic load
Type: BOOK - Published: 1960 - Publisher:

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Effects of Spoiler-slot-deflector Control on the Aerodynamic Characteristics at a Mach Number of 2.01 of a Variable-wing-sweep Configuration with the Outer Wing Panels Swept Back 75°
Language: en
Pages: 20

Effects of Spoiler-slot-deflector Control on the Aerodynamic Characteristics at a Mach Number of 2.01 of a Variable-wing-sweep Configuration with the Outer Wing Panels Swept Back 75°

Authors: Gerald V. Foster
Categories: Aerodynamics, Supersonic
Type: BOOK - Published: 1960 - Publisher:

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Pressure Distributions and Aerodynamic Characteristics of Several Spoiler Controls on a 40 Degree Sweptback Wing at a Mach Number of 1.61
Language: en
Pages: 70

Pressure Distributions and Aerodynamic Characteristics of Several Spoiler Controls on a 40 Degree Sweptback Wing at a Mach Number of 1.61

Authors: Emma Jean Landrum
Categories: Aerofoils
Type: BOOK - Published: 1960 - Publisher:

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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
Language: en
Pages: 38

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

Authors:
Categories:
Type: BOOK - Published: 1960 - Publisher:

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