Investigation At Transonic Speeds Of The Loading Over A 40 Degree Sweptback Wing Having An Aspect Ratio Of 3 A Taper Ratio Of 02 And Naca 65a004 Airfoil Sections

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Investigation at Transonic Speeds of the Loading Over a 45 Degree Sweptback Wing Having an Aspect Ratio of 3, a Taper Ratio of 0.2, and NACA 65A004 Airfoil Sections
Language: en
Pages: 104

Investigation at Transonic Speeds of the Loading Over a 45 Degree Sweptback Wing Having an Aspect Ratio of 3, a Taper Ratio of 0.2, and NACA 65A004 Airfoil Sections

Authors: Jack F. Runckel
Categories: Aerodynamic load
Type: BOOK - Published: 1956 - Publisher:

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An investigation at transonic speeds of the loading over a 45 degree sweptback wing having an aspect ratio of 3, a taper ratio of 0.2, and NACA 65A004 airfoil s
Investigation at Transonic Speeds of the Loading Over a 40 Degree Sweptback Wing Having an Aspect Ratio of 3, a Taper Ratio of 0.2 and NACA 65A004 Airfoil Sections
Language: en
Pages: 93

Investigation at Transonic Speeds of the Loading Over a 40 Degree Sweptback Wing Having an Aspect Ratio of 3, a Taper Ratio of 0.2 and NACA 65A004 Airfoil Sections

Authors: Jack F. Runckel
Categories:
Type: BOOK - Published: 1961 - Publisher:

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Investigation at Transonic Speeds of the Loading Over a 45 Degree Sweptback Wing Having an Aspect Ratio of 3, a Taper Ratio of 0.2, and Naca 65a004 Airfoil Sections
Language: en
Pages: 1

Investigation at Transonic Speeds of the Loading Over a 45 Degree Sweptback Wing Having an Aspect Ratio of 3, a Taper Ratio of 0.2, and Naca 65a004 Airfoil Sections

Authors: JACK F. RUNCKEL
Categories:
Type: BOOK - Published: 1961 - Publisher:

DOWNLOAD EBOOK

An investigation at transonic speeds of the loading over a 45 degree sweptback wing having an aspect ratio of 3, a taper ratio of 0.2, and NACA 65A004 airfoil s
Investigation at Transonic Speeds of Loading Over a 30 Degree Sweptback Wing of Aspect Ratio 3, Taper Ratio 0.2, and NACA 65A004 Airfoil Section Mounted on a Body
Language: en
Pages: 79

Investigation at Transonic Speeds of Loading Over a 30 Degree Sweptback Wing of Aspect Ratio 3, Taper Ratio 0.2, and NACA 65A004 Airfoil Section Mounted on a Body

Authors: Donald D. Arabian
Categories: Aerodynamic load
Type: BOOK - Published: 1957 - Publisher:

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The aerodynamic load characteristics of a wing-body combination were determined experimentally from 0.80 to 1.03 Mach number for angles of attack up to 26 degre
Investigation at Transonic Speeds of Loading Over a 30° Sweptback Wing of Aspect Ratio 3, Taper 0.2, and NACA 65A004 Airfoil Section Mounted on a Body
Language: en
Pages: 79

Investigation at Transonic Speeds of Loading Over a 30° Sweptback Wing of Aspect Ratio 3, Taper 0.2, and NACA 65A004 Airfoil Section Mounted on a Body

Authors: Donald D. Arabian
Categories:
Type: BOOK - Published: 1960 - Publisher:

DOWNLOAD EBOOK