Loads On Wings Due To Spoilers At Subsonic And Transonic Speeds
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Loads on Wings Due to Spoilers at Subsonic and Transonic Speeds
Author | : Alexander D. Hammond |
Publsiher | : Unknown |
Total Pages | : 18 |
Release | : 1955 |
Genre | : Aerodynamic load |
ISBN | : UOM:39015086507038 |
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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 to NASA Technical Publications
Author | : United States. National Aeronautics and Space Administration |
Publsiher | : Unknown |
Total Pages | : 135 |
Release | : 1960-07 |
Genre | : Electronic Book |
ISBN | : STANFORD:36105024165701 |
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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 |
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A Selected Listing of NASA Scientific and Technical Reports for
Author | : Anonim |
Publsiher | : Unknown |
Total Pages | : 818 |
Release | : 1954 |
Genre | : Aeronautics |
ISBN | : UVA:X004173286 |
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NACA Conference on Aircraft Loads Structures and Flutter
Author | : Anonim |
Publsiher | : Unknown |
Total Pages | : 702 |
Release | : 1957 |
Genre | : Aerodynamics |
ISBN | : STANFORD:36105024836160 |
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Aerodynamic Characteristics of a Spoiler slot deflector Control on a 45 Sweptback Wing at Mach Numbers of 1 61 and 2 01
Author | : Douglas R. Lord |
Publsiher | : Unknown |
Total Pages | : 52 |
Release | : 1957 |
Genre | : Aerodynamics |
ISBN | : UOM:39015086466151 |
Download Aerodynamic Characteristics of a Spoiler slot deflector Control on a 45 Sweptback Wing at Mach Numbers of 1 61 and 2 01 Book in PDF, Epub and Kindle
An investigation has been made in the Langley 4- by 4-foot supersonic pressure tunnel at Mach numbers of 1.61 and 2.01 to determine the aerodynamic characteristics of a spoiler-slot-deflector control on a 45 degree sweptback wing having an aspect ratio of 3.5, a taper ratio of 0.3, and an NACA 65A005 airfoil section. The model was equipped with a 15-percent-chord spoiler-slot-deflector extending from 13 o 78 percent of the wing semispan. The spoiler and deflector were hinged along the 60- and 75-percent-chord lines, respectively. Tests were made at a Reynolds number of 3,000,000 (based on the mean aerodynamic chord of the wing) and covered ranges of angles of attack from -3 to 15 degrees, spoiler projections from 0 to 8.0 percent chord, and deflector projections from 0 to 7.6 percent chord.