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Effect Of Leading Edge Chord Extensions On The Aerodynamic Characteristics Of A 45 Degrees Sweptback Wing Fuselage Combination At Mach Numbers Of 040 To 103
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Book Synopsis 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 by : F.E. Jr West
Download or read book 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 published by . This book was released on 1953 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effect of Leading-edge Chord-extensions on the Aerodynamic Characteristics of a 45 Sweptback Wing-fuselage Combination at Mach Numbers of 0.40 to 1.03 by :
Download or read book Effect of Leading-edge Chord-extensions on the Aerodynamic Characteristics of a 45 Sweptback Wing-fuselage Combination at Mach Numbers of 0.40 to 1.03 written by and published by . This book was released on 1953 with total page 43 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis 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 by : Kenneth P. Spreemann
Download or read book 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 published by . This book was released on 1957 with total page 644 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.
Book Synopsis 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 by : Kenneth P. Spreemann
Download or read book 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 published by . This book was released on 1953 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effect of Leading-edge Chord-extensions on Subsonic and Transonic Aerodynamic Characteristics of Three Models Having 45 Degrees Sweptback Wings of Aspect Ratio 4 by : Kenneth W. Goodson
Download or read book 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 published by . This book was released on 1953 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis 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 by : Ellery B. Jr May
Download or read book 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 published by . This book was released on 1951 with total page 25 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Effect of Leading-edge Extensions on the Longitudinal Characteristics at Mach Numbers Up to 0.92 of a Wing-fuselage-tail Combination Having a 40 Degree Sweptback Wing with NACA 64A Thickness Distribution by : Fred B. Sutton
Download or read book The Effect of Leading-edge Extensions on the Longitudinal Characteristics at Mach Numbers Up to 0.92 of a Wing-fuselage-tail Combination Having a 40 Degree Sweptback Wing with NACA 64A Thickness Distribution written by Fred B. Sutton and published by . This book was released on 1956 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effect of Leading-edge Chord-extensions on Subsonic and Transonic Aerodynamic Characteristics of Three Models Having 45 Degree Sweptback Wings of Aspect Ratio 4 by : Kenneth W. Goodson
Download or read book 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 published by . This book was released on 1953 with total page 31 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Longitudinal Aerodynamic Characteristics of a Sweptback Wing-body Combination with and Without End Plates at Mach Numbers from 0.40 to 0.93 by : W. P. Henderson
Download or read book The Longitudinal Aerodynamic Characteristics of a Sweptback Wing-body Combination with and Without End Plates at Mach Numbers from 0.40 to 0.93 written by W. P. Henderson and published by . This book was released on 1960 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of Wing Planform on the Aerodynamic Characteristics of a Wing-body-tail Model at Mach Numbers 1.57, 2.16, and 2.87 by : Royce L. McKinney
Download or read book Effects of Wing Planform on the Aerodynamic Characteristics of a Wing-body-tail Model at Mach Numbers 1.57, 2.16, and 2.87 written by Royce L. McKinney and published by . This book was released on 1965 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of Wing-crank, Leading-edge Chord Extensions and Horizontal-tail Height on the Longitudinal Stability of Swept-wing Models at Mach Numbers from 0.6 to 1.4 by : Roy M. Wakefield
Download or read book Effects of Wing-crank, Leading-edge Chord Extensions and Horizontal-tail Height on the Longitudinal Stability of Swept-wing Models at Mach Numbers from 0.6 to 1.4 written by Roy M. Wakefield and published by . This book was released on 1959 with total page 120 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Transonic Investigation of Changing Indentation Design Mach Number on the Aerodynamic Characteristics of a 45 Degree Sweptback-wing-body Combination Designed for High Performance by : Donald L. Loving
Download or read book A Transonic Investigation of Changing Indentation Design Mach Number on the Aerodynamic Characteristics of a 45 Degree Sweptback-wing-body Combination Designed for High Performance written by Donald L. Loving and published by . This book was released on 1961 with total page 92 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effect of Wing Leading-edge Shape on Aerodynamic Characteristics of a 67 ̊swept Wing-body Model at Mach 1.50 to 4.63 by : Robert G. Kyle
Download or read book Effect of Wing Leading-edge Shape on Aerodynamic Characteristics of a 67 ̊swept Wing-body Model at Mach 1.50 to 4.63 written by Robert G. Kyle and published by . This book was released on 1966 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of Leading-edge Chord Extensions and an All-movable Horizontal Tail on the Aerodynamic Characteristics of a Wing-body Combination Employing a Triangular Wing of Aspect Ratio 3 Mounted in a High Position at Subsonic and Supersonic Speeds by : Benton E. Wetzel
Download or read book Effects of Leading-edge Chord Extensions and an All-movable Horizontal Tail on the Aerodynamic Characteristics of a Wing-body Combination Employing a Triangular Wing of Aspect Ratio 3 Mounted in a High Position at Subsonic and Supersonic Speeds written by Benton E. Wetzel and published by . This book was released on 1954 with total page 35 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effect of Leading-edge Droop on the Aerodynamic and Loading Characteristics of a 4-percent-thick Unswept-wing-fuselage Combination at Transonic Speeds by : James W. Schmeer
Download or read book Effect of Leading-edge Droop on the Aerodynamic and Loading Characteristics of a 4-percent-thick Unswept-wing-fuselage Combination at Transonic Speeds written by James W. Schmeer and published by . This book was released on 1956 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was conducted in the Langley 16-foot transonic tunnel to determine the effects of leading-edge droop on the aerodynamic and loading characteristics of an unswept wing with a taper ratio of 0.5, an aspect ratio of 4, an NACA 65A004 airfoil sections parallel to the plane of symmetry. The leading edge of the wing was drooped both 6 and 10 degrees about the 17-percent-chord line, full span. Force, moment, and pressure measurements were obtained at Mach numbers from 0.60 to 1.05 and angles of attack, depending on Mach number, from approximately 0 to 16 degrees. The Reynolds number, based on the mean aerodynamic chord, varied from 4,600,000 to 6,300,000.
Book Synopsis Effects of Leading-edge Slats on the Aerodynamic Characteristics of a 45 Degree Sweepback Wing-fuselage Configuration at Mach Numbers of 0.4 to 1.03 by : Jack F. Runckel
Download or read book Effects of Leading-edge Slats on the Aerodynamic Characteristics of a 45 Degree Sweepback Wing-fuselage Configuration at Mach Numbers of 0.4 to 1.03 written by Jack F. Runckel and published by . This book was released on 1953 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt:
