An Experimental Investigation of the Aerodynamic Characteristics of a Thin Supercritical Airfoil with Small Leading Edge Radius PDF Download
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Author: Richard L. Perry (CAPT, USAF.)
Publisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 150
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Book Description
Author: Richard L. Perry (CAPT, USAF.)
Publisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 150
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Book Description
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 116
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Book Description
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 396
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Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 620
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Book Description
Author: Charles D. Harris
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 80
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Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1006
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Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 654
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Book Description
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 258
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Book Description
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 996
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Book Description
Author: Dean R. Chapman
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 852
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Book Description
The pressres acting on the base of blunt-trailing-edge airfoils have been measured at Mach numbers of 1.25, 1.5, 2.0, and 3.1 and at Reynolds numbers from 0.2 to 3.8 million. Data are presented for 29 profiles both with laminar and with turbulent boundary layers approaching the trailing edges of the wings. The base pressure is found to be a function primarily of Mach number and the ratio of the boundary layer thickeness at the trailing edge to the trailing-edge thickness.
