Data for a NACA 23012C Aerofoil Pitched about its Quarter Chord Axis. Volume I: Pressure data from static and ramp function tests, with photographs of oil-flow visualisation tests

Gracey, M.W. and Galbraith, R.A.M. (1989) Data for a NACA 23012C Aerofoil Pitched about its Quarter Chord Axis. Volume I: Pressure data from static and ramp function tests, with photographs of oil-flow visualisation tests. Technical Report. Department of Aerospace Engineering, University of Glasgow.

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Abstract

Herein is presented the collected data for tests in which a NACA 23012C aerofoil was subjected to a variety of ramp type displacements in pitch about the quarter chord position at low Reynolds numbers. In addition, the results of static tests and oil-flow visualisation experiments on the aerofoil are displayed.

Item Type:Research Reports or Papers (Technical Report)
Additional Information:"NACA 23012C - Volume I" at head of title.
Status:Published
Glasgow Author(s) Enlighten ID:Galbraith, Professor Roderick
Authors: Gracey, M.W., and Galbraith, R.A.M.
College/School:College of Science and Engineering > School of Engineering > Aerospace Sciences
Publisher:Department of Aerospace Engineering, University of Glasgow
Copyright Holders:Copyright © 1989 Department of Aerospace Engineering, University of Glasgow
Publisher Policy:Reproduced with the permission of the Department

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