Niven, A.J. and Galbraith, R.A.M. (1984) A Design Procedure to Modify the Trailing Edge Upper Surface Pressure Gradient of a Given Aerofoil. G.U. Aero Report 8408. Technical Report. Department of Aeronautics and Fluid Mechanics, University of Glasgow.
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Text (scanned version of the original print report)
185458.pdf - Published Version 11MB |
Abstract
Summary: Little is known about the detailed flow on the upper surface of aerofoils, prone to trailing edge separation, during the process of dynamic stall. The present report describes a method whereby the pressure gradient on the trailing edge upper surface of a given aerofoil may be modified to either enhance or reduce such separations, for a given section, whilst retaining the leading edge pressure distribution.
| Item Type: | Research Reports or Papers (Technical Report) |
|---|---|
| Status: | Published |
| Glasgow Author(s) Enlighten ID: | Galbraith, Professor Roderick |
| Authors: | Niven, A.J., and Galbraith, R.A.M. |
| College/School: | College of Science and Engineering > School of Engineering > Autonomous Systems and Connectivity |
| 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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