An Experimental Study Of A Method Of Designing The Sweptback Wing Fuselage Juncture For Reducing The Drag At Transonic Speeds
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An Experimental Study of a Method of Designing the Sweptback wing Fuselage Juncture for Reducing the Drag at Transonic Speeds
Author | : Robert R. Howell |
Publsiher | : Unknown |
Total Pages | : 30 |
Release | : 1955 |
Genre | : Aerodynamics, Transonic |
ISBN | : UOM:39015086465757 |
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An investigation has been made in the Langley transonic blowdown tunnel at Mach numbers between 0.84 and 1.32 at an angle of attack of zero degrees to determine the pressure-drag reductions attainable on a sweptback-wing - fuselage configuration tested consisted of a 45 degree sweptback wing of aspect ratio 4 in combination with a fineness-ratio-6.7 body. The results indicate that the pressure drag of a practical sweptback-wing - body configuration depends on the body cross-sectional shape as well as upon the longitudinal distribution of cross-sectional area.
Effect of Streamline Contouring in the Wing fuselage Juncture in Combination with the Supersonic Area Rule on a Sweptback wing fuselage Configuration of High Fineness Ratio
Author | : Charles D. Trescot |
Publsiher | : Unknown |
Total Pages | : 24 |
Release | : 1960 |
Genre | : Aerodynamics, Supersonic |
ISBN | : UIUC:30112106587964 |
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Transonic Investigation at Lifting Conditions of Streamline Contouring in the Sweptback wing fuselage Juncture in Combination with the Transonic Area Rule
Author | : William E. Palmer,Robert R. Howell,Albert L. Braslow |
Publsiher | : Unknown |
Total Pages | : 40 |
Release | : 1956 |
Genre | : Aerodynamics, Transonic |
ISBN | : UOM:39015086507111 |
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Progress in Aeronautical Sciences
Author | : Antonio Ferri,D. Küchemann,L. H. G. Sterne |
Publsiher | : Elsevier |
Total Pages | : 250 |
Release | : 2016-06-30 |
Genre | : Technology & Engineering |
ISBN | : 9781483149424 |
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Progress in Aeronautical Sciences, Volume 3 deals with topics in the field of aerodynamics. The book covers topics on aerodynamic design, propulsion systems, hypersonic flows laboratories, and gust research. The text is composed of four articles. The first article presents a review of the aspects of aerodynamic design of swept-winged aircraft. The second paper surveys the applications of ducted propellers. Critical reviews of experimental hypersonic facilities are provided in Chapter 3. The last paper focuses on the meteorological and aeronautical aspects of atmospheric turbulence. Aeronautical engineers, pilots, aviators, and students in the field of aerodynamic design will find this book invaluable.
NASA Technical Note
Author | : Anonim |
Publsiher | : Unknown |
Total Pages | : 534 |
Release | : 1960 |
Genre | : Electronic Book |
ISBN | : MINN:31951000845678J |
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Index of NASA Technical Publications
Author | : United States. National Aeronautics and Space Administration |
Publsiher | : Unknown |
Total Pages | : 448 |
Release | : 1960 |
Genre | : Aeronautics |
ISBN | : UIUC:30112032439504 |
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Index of NASA Technical Publications
Author | : Anonim |
Publsiher | : Unknown |
Total Pages | : 494 |
Release | : 1959 |
Genre | : Aeronautics |
ISBN | : IND:30000099775029 |
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Index of NACA Technical Publications
Author | : United States. National Advisory Committee for Aeronautics |
Publsiher | : Unknown |
Total Pages | : 388 |
Release | : 1959 |
Genre | : Aeronautics |
ISBN | : UCBK:C029901327 |
Download Index of NACA Technical Publications Book in PDF, Epub and Kindle