Pressure Distributions And Aerodynamic Characteristics Of Several Spoiler Controls On A 40 Degree Sweptback Wing At A Mach Number Of 161

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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

Author	: Emma Jean Landrum
Publisher	:
Total Pages	: 70
Release	: 1960
ISBN-10	: UIUC:30112106589283
ISBN-13	:
Rating	: 4/5 ( Downloads)

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Book Synopsis Pressure Distributions and Aerodynamic Characteristics of Several Spoiler Controls on a 40 Degree Sweptback Wing at a Mach Number of 1.61 by : Emma Jean Landrum

Download or read book Pressure Distributions and Aerodynamic Characteristics of Several Spoiler Controls on a 40 Degree Sweptback Wing at a Mach Number of 1.61 written by Emma Jean Landrum and published by . This book was released on 1960 with total page 70 pages. Available in PDF, EPUB and Kindle. Book excerpt:

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

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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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

Language: en
Pages: 52

Effects of Overhang Balance on the Hinge-moment and Effectiveness Characteristics of an Unswept Trailing-edge Control on a 60 Degree Delta Wing at Transonic and Supersonic Speeds

Authors: Lawrence D. Guy

Categories: Aerodynamics, Supersonic

Type: BOOK - Published: 1954 - Publisher:

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A wind-tunnel investigation has been made of two unswept, partial-span, flap-type controls (differing only in hinge-line location) mounted on a 60 degree delta

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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Language: en
Pages: 86

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

Authors: Alexander D. Hammond

Categories: Airplanes

Type: BOOK - Published: 1963 - Publisher:

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