Transonic Wind-tunnel Investigation of an Unswept Wing in Combination with a Systematic Series of Four Bodies PDF Download
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Author: Bruce B. Estabrooks
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 34
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Book Description
Author: Bruce B. Estabrooks
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 34
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Book Description
Author: Donald L. Loving
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 52
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Book Description
Author: Melvin M. Carmel
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 50
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Book Description
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 388
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Book Description
Author: Donald L. Loving
Publisher:
ISBN:
Category :
Languages : en
Pages : 43
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Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 818
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Author: United States. Wright Air Development Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1268
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Author: Bruce B. Estabrooks
Publisher:
ISBN:
Category :
Languages : en
Pages : 23
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Author: Thomas C. Kelly
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 86
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Book Description
Pressure data have been obtained in the Langley 8-foot transonic tunnel at Mach numbers from 0.80 to 1.115 and angles of attack from 0 to 20 degrees for wing-body configurations employing a thin trapezoidal wing in combination with basic and indented bodies. The wing had 26.6 degrees sweepback of the quarter-chord line, an aspect ratio of 2.61, a taper ratio of 0.211, and 2-percent-thick symmetrical circular-arc airfoil sections parallel to the plane of symmetry. Results are also presented for the basic body alone. Reynolds numbers for the tests were on the order of 2,600,000, based on the wing mean aerodynamic chord.
Author: Thomas C. Kelly
Publisher:
ISBN:
Category :
Languages : en
Pages : 22
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Book Description
