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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Text (scanned version of the original print report)
1838016.pdf - Published Version 90MB |
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 > Autonomous Systems and Connectivity |
| 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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