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
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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
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Author : Kenneth P. Spreemann
language : en
Publisher:
Release Date : 1957
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 written by Kenneth P. Spreemann and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1957 with Airplanes categories.
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
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Author : Kenneth P. Spreemann
language : en
Publisher:
Release Date : 1957
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 written by Kenneth P. Spreemann and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1957 with Airplanes categories.
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 fences on the aerodynamic characteristics of a wing-fuselage configuration with a 45 degree sweptback wing of aspect ratio 4, taper ratio 0.3, and NACA 65A006 airfoil sections. The investigation was made in the Langley high-speed 7- by 10-foot tunnel over a Mach number range of 0.40 to 0.93 and an angle-of-attack range of about -2 degrees to 24 degrees. Lift, drag, and pitching-moment data were obtained for all configurations. From overall considerations of stability and performance it appears that with the model of this investigation the 6 degree full-span leading-edge flaps in combination with the chord-extension over the outboard 35 percent of the span, with or without leading-edge camber, would be the most desirable configuration.
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
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Author : Kenneth P. Spreemann
language : en
Publisher:
Release Date : 1953
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 written by Kenneth P. Spreemann and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1953 with categories.
Effects Of Fences Leading Edge Chord Extensions Bound Layer Ramps And Trailing Edge Flaps On The Longitudinal Stability Of A Twisted And Cambered 60 Sweptback Wing Indented Body Configuration At Transonic Speeds
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Author : Thomas L. Fischetti
language : en
Publisher:
Release Date : 1954
Effects Of Fences Leading Edge Chord Extensions Bound Layer Ramps And Trailing Edge Flaps On The Longitudinal Stability Of A Twisted And Cambered 60 Sweptback Wing Indented Body Configuration At Transonic Speeds written by Thomas L. Fischetti and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1954 with Aerodynamics, Transonic categories.
Investigation Of The Effects Of Leading Edge Chord Extensions On The Aerodynamic And Control Characteristics Of Two Sweptback Wings At Mach Numbers Of 1 41 1 62 And 1 96
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Author : Ellery B. Jr May
language : en
Publisher:
Release Date : 1951
Investigation Of The Effects Of Leading Edge Chord Extensions On The Aerodynamic And Control Characteristics Of Two Sweptback Wings At Mach Numbers Of 1 41 1 62 And 1 96 written by Ellery B. Jr May and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1951 with categories.
Experimental Investigation At High Subsonic Speeds Of The Effects Of Leading Edge Radius On The Aerodynamic Characteristics Of A Sweptback Wing Fuselage Combination With Leading Edge Flaps And Chord Extensions
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Author : Kenneth P. Spreemann
language : en
Publisher:
Release Date : 1955
Experimental Investigation At High Subsonic Speeds Of The Effects Of Leading Edge Radius On The Aerodynamic Characteristics Of A Sweptback Wing Fuselage Combination With Leading Edge Flaps And Chord Extensions written by Kenneth P. Spreemann and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1955 with Airplanes categories.
A limited investigation was made at high subsonic speeds to determine the effects of a wing leading-edge radius on the aerodynamic characteristics of a sweptback-wing-fuselage combination with leading-edge flaps and chord-extensions. The basic wing had 45 degree sweepback, aspect ratio 4, taper ratio 0.3, and NACA 65A006 airfoil section. The leading-edge shapes considered consisted of a sharp leading edge, a normal airfoil leading edge, and a leading edge formed by using three times the normal radius and fairing the new nose contour smoothly into the normal airfoil. The investigation was made in the Langley high-speed 7- by 10-foot tunnel over a Mach number range of 0.80 to 0.92 and an angle-of-attack range of -2 to 24 degrees. Lift, drag, and pitching-moment data were obtained for all configurations with leading-edge flap deflections of 0 to 6 degrees.
Investigation Of The Effects Of Leading Edge Flaps On The Aerodynamic Characteristics In Pitch At Mach Numbers From 0 40 To 0 93 Of A Wing Fuselage Configuration With A 45 Degree Sweptback Wing Of Aspect Ratio 4
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Author : Kenneth P. Spreemann
language : en
Publisher:
Release Date : 1953
Investigation Of The Effects Of Leading Edge Flaps On The Aerodynamic Characteristics In Pitch At Mach Numbers From 0 40 To 0 93 Of A Wing Fuselage Configuration With A 45 Degree Sweptback Wing Of Aspect Ratio 4 written by Kenneth P. Spreemann and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1953 with categories.
Effect Of Leading Edge Chord Extensions On Subsonic And Transonic Aerodynamic Characteristics Of Three Models Having 45 Degrees Sweptback Wings Of Aspect Ratio 4
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Author : Kenneth W. Goodson
language : en
Publisher:
Release Date : 1953
Effect Of Leading Edge Chord Extensions On Subsonic And Transonic Aerodynamic Characteristics Of Three Models Having 45 Degrees Sweptback Wings Of Aspect Ratio 4 written by Kenneth W. Goodson and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1953 with categories.
Effect Of Leading Edge Chord Extensions On The Aerodynamic Characteristics Of A 45 Degrees Sweptback Wing Fuselage Combination At Mach Numbers Of 0 40 To 1 03
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Author : F.E. Jr West
language : en
Publisher:
Release Date : 1953
Effect Of Leading Edge Chord Extensions On The Aerodynamic Characteristics Of A 45 Degrees Sweptback Wing Fuselage Combination At Mach Numbers Of 0 40 To 1 03 written by F.E. Jr West and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1953 with categories.
Effect Of Leading Edge Chord Extensions On Subsonic And Transonic Aerodynamic Characteristics Of Three Models Having 45 Degree Sweptback Wings Of Aspect Ratio 4
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Author : Kenneth W. Goodson
language : en
Publisher:
Release Date : 1953
Effect Of Leading Edge Chord Extensions On Subsonic And Transonic Aerodynamic Characteristics Of Three Models Having 45 Degree Sweptback Wings Of Aspect Ratio 4 written by Kenneth W. Goodson and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1953 with categories.