The Collected Data for Ramp Function Tests on a NACA 23012 Aerofoil. Volume 1: Description and Pressure Data. G.U. Aero Report 8413

Seto, L.Y. and Galbraith, R.A.M. (1984) The Collected Data for Ramp Function Tests on a NACA 23012 Aerofoil. Volume 1: Description and Pressure Data. G.U. Aero Report 8413. Technical Report. Department of Aeronautics and Fluid Mechanics, University of Glasgow.

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Abstract

Summary: Here in is presented the collected data for tests in which a NACA 23012 aerofoil was subjected to a variety of ramp type displacements in pitch about the quarter chord position. The data clearly illustrates the effect of reduced frequency on the aerofoil characteristics and the chordal pressure distribution at the midspan position of the aerofoil model.

Item Type:Research Reports or Papers (Technical Report)
Status:Published
Glasgow Author(s) Enlighten ID:Galbraith, Professor Roderick
Authors: Seto, L.Y., and Galbraith, R.A.M.
College/School:College of Science and Engineering > School of Engineering > Aerospace Sciences
Publisher:Department of Aeronautics and Fluid Mechanics, University of Glasgow
Copyright Holders:Copyright © 1984 Department of Aeronautics and Fluid Mechanics, University of Glasgow
Publisher Policy:Reproduced with the permission of the Department
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