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:
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.
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:
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 of 0 40 to 0 93 of a 45 Sweptback Wing of Aspect Ratio 4 written by Kenneth P. Spreemann and published by . This book was released on 1957 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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:
Download or read book Index to NASA Technical Publications written by United States. National Aeronautics and Space Administration and published by . This book was released on 1960-07 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
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:
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:
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:
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:
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:
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:
Download or read book Aeronautical Engineering Review written by and published by . This book was released on 1957 with total page 844 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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:
Download or read book Aero space Engineering written by and published by . This book was released on 1958 with total page 1508 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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:
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:
