Investigation Of The Variation Of Maximum Lift For A Pitching Airplane Model And Comparison With Flight Results

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Investigation of the Variation of Maximum Lift for a Pitching Airplane Model and Comparison with Flight Results

Author : Paul W. Harper,Roy E. Flanigan
Publisher : Unknown
Page : 706 pages
File Size : 47,9 Mb
Release : 1948
Category : Airplanes
ISBN : STANFORD:36105024795820

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Investigation of the Variation of Maximum Lift for a Pitching Airplane Model and Comparison with Flight Results by Paul W. Harper,Roy E. Flanigan Pdf

Apparatus was developed which utilized a pitching airplane model to determine maximum wing loads as a function of the rate of change of angle of attack. In order to evaluate the pitching-model technique, the maximum lift coefficient was determined as a function of the rate of change of angle of attack over a Mach number range from approximately 0.2 to 0.6 in wind-tunnel tests of a 1/20-scale model of a conventional single-engine fighter airplane and was conpared with existing flight data of this airplane. The wind-tunnel and flight results were found to be in good agreement.

Technical Note - National Advisory Committee for Aeronautics

Author : United States. National Advisory Committee for Aeronautics
Publisher : Unknown
Page : 1070 pages
File Size : 48,8 Mb
Release : 1950
Category : Aeronautics
ISBN : RUTGERS:39030037542299

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Technical Note - National Advisory Committee for Aeronautics by United States. National Advisory Committee for Aeronautics Pdf

Index of NACA Technical Publications

Author : United States. National Advisory Committee for Aeronautics
Publisher : Unknown
Page : 616 pages
File Size : 40,7 Mb
Release : 1949
Category : Aeronautics
ISBN : MSU:31293201271115

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Index of NACA Technical Publications by United States. National Advisory Committee for Aeronautics Pdf

Technical Note

Author : Anonim
Publisher : Unknown
Page : 460 pages
File Size : 42,8 Mb
Release : 1950
Category : Aeronautics
ISBN : UIUC:30112008553551

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Technical Note by Anonim Pdf

Velocity Distribution on Wing Sections of Arbitrary Shape in Compressible Potential Flow

Author : Lipman Bers
Publisher : Unknown
Page : 700 pages
File Size : 45,5 Mb
Release : 1950
Category : Aerofoils
ISBN : STANFORD:36105024795853

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Velocity Distribution on Wing Sections of Arbitrary Shape in Compressible Potential Flow by Lipman Bers Pdf

The method of computing velocity and pressure distributions along wing profiles under the assumption of the simplified density-speed relation, outlined in NACA Technical Note 1006, is extended to the case of a nonsymmetrical profile and a flow with circulation. The shape of the profile, the speed of the undisturbed flow, and a parameter determing the angle of attack may be prescribed. The problem is reduced to a nonlinear integral equation which can be solved numerical by an iteration method. A numerical example is given.

Applied Mechanics Reviews

Author : Anonim
Publisher : Unknown
Page : 1196 pages
File Size : 40,6 Mb
Release : 1963
Category : Mechanics, Applied
ISBN : UCAL:C2682418

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Applied Mechanics Reviews by Anonim Pdf

Report

Author : Anonim
Publisher : Unknown
Page : 880 pages
File Size : 40,8 Mb
Release : 1922
Category : Aeronautics
ISBN : UIUC:30112112405557

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Report by Anonim Pdf

Report - National Advisory Committee for Aeronautics

Author : United States. National Advisory Committee for Aeronautics
Publisher : Unknown
Page : 808 pages
File Size : 48,7 Mb
Release : 1930
Category : Aeronautics
ISBN : CORNELL:31924089862357

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Report - National Advisory Committee for Aeronautics by United States. National Advisory Committee for Aeronautics Pdf

Annual Report - National Advisory Committee for Aeronautics

Author : United States. National Advisory Committee for Aeronautics
Publisher : Unknown
Page : 128 pages
File Size : 49,7 Mb
Release : 1957
Category : Aeronautics
ISBN : STANFORD:36105024166147

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Annual Report - National Advisory Committee for Aeronautics by United States. National Advisory Committee for Aeronautics Pdf

Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.

Technical Information Pilot

Author : Anonim
Publisher : Unknown
Page : 332 pages
File Size : 48,6 Mb
Release : 1950
Category : Science
ISBN : STANFORD:36105010854177

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Technical Information Pilot by Anonim Pdf

Research Abstracts

Author : United States. National Advisory Committee for Aeronautics
Publisher : Unknown
Page : 568 pages
File Size : 53,8 Mb
Release : 1951
Category : Aeronautics
ISBN : IND:30000088900174

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Research Abstracts by United States. National Advisory Committee for Aeronautics Pdf