A Wind-tunnel Investigation of the Wing Loads Due to Deflected Inboard Ailerons on a 45 Degree Sweptback Wing at Transonic Speeds PDF Download
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Author: Astwood R. Jr Heath
Publisher:
ISBN:
Category :
Languages : en
Pages : 100
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Book Description
Author: Astwood R. Jr Heath
Publisher:
ISBN:
Category :
Languages : en
Pages : 100
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Book Description
Author: Charles F. Whitcomb
Publisher:
ISBN:
Category :
Languages : en
Pages : 286
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Book Description
Author: Donald L. Loving
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 52
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Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 1074
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Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Author: Charles F. Whitcomb
Publisher:
ISBN:
Category :
Languages : en
Pages : 282
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Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 448
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Author:
Publisher:
ISBN:
Category : Industrial arts
Languages : en
Pages : 1048
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Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 1196
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Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 818
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Author: Jack F. Runckel
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 104
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Book Description
An investigation at transonic speeds of the loading over a 45 degree sweptback wing having an aspect ratio of 3, a taper ratio of 0.2, and NACA 65A004 airfoil sections has been conducted in the Langley16-foot transonic tunnel. Pressure measurements on the wing-body combination were obtained at angles of attack from 0 to 26 degrees at Mach numbers from 0.80 to 0.98 and from 0 to about 12 degrees at Mach numbers from 1.00 to 1.05. Reynolds number, based on the wing mean aerodynamic chord, varied from 7,000,000 to 8,500,000 over the test Mach number range.
