Experimental Effects of Wing Location on Wing-body Pressures at Supersonic Speeds PDF Download
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Author: Jerry M. Allen
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 204
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Book Description
Author: Jerry M. Allen
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 204
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Book Description
Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781723574276
Category :
Languages : en
Pages : 204
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Book Description
An experimental study was performed at supersonic speeds to measure wing and body spanwise pressure distributions on an axisymmetric-body delta wing model on which the wing vertical location on the body was systematically varied from low- to high-mounted positions. In addition, for two of these positions both horizontal and radial wing angular orientations relative to the body were tested, and roll angle effects were investigated for one of the positions. Seven different wing-body configurations and a body-alone configuration were studied. The test was conducted at Mach numbers from 1.70 to 2.86 at angles of attack from about -4 deg to 24 deg. Pressure orifices were located at three longitudinal stations on each wing-body model, and at each station the orifices were located completely around the body, along the lower surface of the right wing (looking upstream), and along the upper surface of the left wing. All pressure coefficient data are tabulated and selected samples are shown graphically to illustrate the effects of the test variables. The effects of angle of attack, roll angle, Mach number, longitudinal station, wing vertical location, wing angular orientation, and wing-body juncture are analyzed. The vertical location of the wing on the body had a very strong effect on the body pressures. For a given angle of attack at a roll angle of 0 deg, the pressures were virtually constant in the spanwise direction across the windward surfaces of the wing-body combination. Pressure-relieving, channeling, and vortex effects were noted in the data. Allen, Jerry M. and Watson, Carolyn B. Langley Research Center NASA-TM-4434, L-17148, NAS 1.15:4434 RTOP 505-59-30-01...
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 556
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Author: A. Gerald Rainey
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 316
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Author: Abe Silverstein
Publisher:
ISBN:
Category : Aerodynamic measurements
Languages : en
Pages : 112
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Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1794
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Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 96
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1138
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Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages :
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Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
Author: Library of Congress. Science and Technology Division
Publisher:
ISBN:
Category : Military research
Languages : en
Pages : 1196
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