An Experimental Investigation of a Mach 3.0 High-speed Civil Transport at Supersonic Speeds PDF Download
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Author: Gloria Hernandez
Publisher:
ISBN:
Category : Aeronautics, Commercial
Languages : en
Pages : 98
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Book Description
Author: Gloria Hernandez
Publisher:
ISBN:
Category : Aeronautics, Commercial
Languages : en
Pages : 98
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Book Description
Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 704
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Category : Government publications
Languages : en
Pages :
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ISBN:
Category : Government publications
Languages : en
Pages : 752
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Author: Gloria Hernandez
Publisher:
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Category : Leading edge flaps
Languages : en
Pages : 112
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Category : Science
Languages : en
Pages : 60
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Category :
Languages : en
Pages : 96
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Author: United States. National Aeronautics and Space Administration
Publisher:
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Category : Aeronautics
Languages : en
Pages : 60
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Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 538
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Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781722182328
Category :
Languages : en
Pages : 98
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Book Description
An experimental study was conducted to determine the aerodynamic characteristics of a proposed high speed civil transport. This configuration was designed to cruise at Mach 3.0 and sized to carry 250 passengers for 6500 n.mi. The configuration consists of a highly blended wing body and features a blunt parabolic nose planform, a highly swept inboard wing panel, a moderately swept outboard wing panel, and a curved wingtip. Wind tunnel tests were conducted in the Langley Unitary Plan Wind Tunnel on a 0.0098-scale model. Force, moment, and pressure data were obtained for Mach numbers ranging from 1.6 to 3.6 and at angles of attack ranging from -4 to 10 deg. Extensive flow visualization studies (vapor screen and oil flow) were obtained in the experimental program. Both linear and advanced computational fluid dynamics (CFD) theoretical comparisons are shown to assess the ability to predict forces, moments, and pressures on configurations of this type. In addition, an extrapolation of the wind tunnel data, based on empirical principles, to full-scale conditions is compared with the theoretical aerodynamic predictions. Hernandez, Gloria and Covell, Peter F. and Mcgraw, Marvin E., Jr. Langley Research Center...
