Twisted Wing
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Span Loadings Due to Wing Twist at Transonic and Supersonic Speeds
Author | : Frederick C. Grant |
Publsiher | : Unknown |
Total Pages | : 18 |
Release | : 1957 |
Genre | : Aerodynamic load |
ISBN | : UOM:39015086466110 |
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Two similar tapered sweptback plan forms with the same two spanwise variations of twist have been tested in the Mach number range from 0.8 to 2.0. The test results showed, in general, rather good agreement with theoretical predictions of the incremental span loadings due to twist for zero angle of attack. The measured incremental span loadings due to twist generally diminished with increasing angle of attack through the Mach number range. At a Mach number of 0.9, the incremental loadings progressively vanished from the tip inboard with increasing angle of attack. For the highest angles of attack (about 20 degrees) at Mach number 0.9, there was no difference in the span loadings of the flat and twisted wings. At a higher supersonic speeds, a similar vanishing at the tips of the incremental loading due to twist was starting at the highest angles of attack (near 20 degrees).
The Elastic Twist of Straight Wings for Symmetrical Load Conditions
Author | : Walther Gustav Carl Boccius |
Publsiher | : Unknown |
Total Pages | : 68 |
Release | : 1948 |
Genre | : Airplanes |
ISBN | : UOM:39015104977502 |
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Transonic and Supersonic Wind tunnel Tests of Wing body Combinations Designed for High Efficiency at a Mach Number of 1 41
Author | : Frederick C. Grant,John R. Sevier |
Publsiher | : Unknown |
Total Pages | : 86 |
Release | : 1960 |
Genre | : Aerodynamics |
ISBN | : UIUC:30112106689315 |
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Fixed Wing Flight
Author | : United States. Department of the Army |
Publsiher | : Unknown |
Total Pages | : 366 |
Release | : 1980 |
Genre | : Flight training |
ISBN | : SRLF:D0002375616 |
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Wind Tunnel Investigation at Low Speed of a Twisted and Cambered Wing Swept Back 63 Degrees with Vortex Generators and Fences
Author | : James A. Weilberg |
Publsiher | : Unknown |
Total Pages | : 64 |
Release | : 1952 |
Genre | : Electronic Book |
ISBN | : NASA:31769000420458 |
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Wing Theory
Author | : Robert Thomas Jones |
Publsiher | : Princeton University Press |
Total Pages | : 227 |
Release | : 2014-07-14 |
Genre | : Technology & Engineering |
ISBN | : 9781400860777 |
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Originator of many of the theories used in modern wing design, Robert T. Jones surveys the aerodynamics of wings from the early theories of lift to modern theoretical developments. This work covers the behavior of wings at both low and high speeds, including the range from very low Reynolds numbers to the determination of minimum drag at supersonic speed. Emphasizing analytical techniques, Wing Theory provides invaluable physical principles and insights for advanced students, professors, and aeronautical engineers, as well as for scientists involved in computational approaches to the subject. This book is based on over forty years of theoretical and practical work performed by the author and other leading researchers in the field of aerodynamics. Originally published in 1990. The Princeton Legacy Library uses the latest print-on-demand technology to again make available previously out-of-print books from the distinguished backlist of Princeton University Press. These editions preserve the original texts of these important books while presenting them in durable paperback and hardcover editions. The goal of the Princeton Legacy Library is to vastly increase access to the rich scholarly heritage found in the thousands of books published by Princeton University Press since its founding in 1905.
Transonic Aerodynamic Characteristics of a Tailless Fixed wing Supersonic Transport Model
Author | : Edward J. Ray,Robert T. Taylor |
Publsiher | : Unknown |
Total Pages | : 84 |
Release | : 1966 |
Genre | : Aerodynamics, Transonic |
ISBN | : UIUC:30112106659847 |
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NASA Technical Note
Author | : Anonim |
Publsiher | : Unknown |
Total Pages | : 242 |
Release | : 1962 |
Genre | : Electronic Book |
ISBN | : MINN:31951000845745U |
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