Related Books

Investigation of the Effects of Leading-edge Chord-extensions and Fences in Combination with Leading-edge Flaps on the Aerodynamic Characteristics at Mach Numbers from 0.40 to 0.93 of a 45 Degree Sweptback Wing of Aspect Ratio 4
Language: en
Pages: 644

Investigation of the Effects of Leading-edge Chord-extensions and Fences in Combination with Leading-edge Flaps on the Aerodynamic Characteristics at Mach Numbers from 0.40 to 0.93 of a 45 Degree Sweptback Wing of Aspect Ratio 4

Authors: Kenneth P. Spreemann
Categories: Airplanes
Type: BOOK - Published: 1957 - Publisher:

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This investigation was made to determine the effects of 6 degree full-span and 3 degree partial-span leading-edge flaps in combination with chord-extensions or
Investigation of the Effects of Leading-edge Chord-extensions and Fences in Combination with Leading-edge Flaps on the Aerodynamic Characteristics at Mach Numbers of 0.40 to 0.93 of a 45© Sweptback Wing of Aspect Ratio 4
Language: en
Pages: 56

Investigation of the Effects of Leading-edge Chord-extensions and Fences in Combination with Leading-edge Flaps on the Aerodynamic Characteristics at Mach Numbers of 0.40 to 0.93 of a 45© Sweptback Wing of Aspect Ratio 4

Authors: Kenneth P. Spreemann
Categories: Airplanes
Type: BOOK - Published: 1957 - Publisher:

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Aero/space Engineering
Language: en
Pages: 1508

Aero/space Engineering

Authors:
Categories: Aeronautics
Type: BOOK - Published: 1958 - Publisher:

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Aeronautical Engineering Review
Language: en
Pages: 1846

Aeronautical Engineering Review

Authors:
Categories: Aeronautics
Type: BOOK - Published: 1957 - Publisher:

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Airfoil Design and Data
Language: en
Pages: 569

Airfoil Design and Data

Authors: Richard Eppler
Categories: Technology & Engineering
Type: BOOK - Published: 2012-12-06 - Publisher: Springer Science & Business Media

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This detailed book describes a procedure for the design and analysis of subsonic airfoils. Contains 116 new airfoils for a wide range of Reynolds numbers and ap