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

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Aerodynamic Characteristics of a Spoiler-slot-deflector Control on a 45 Degree Sweptback Wing at Mach Numbers of 1.61 and 2.01
Language: en
Pages: 47