The estimation of aerodynamic forces on flat plate aerofoils at hypersonic and supersonic speed
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Published:2012-11
Issue:1185
Volume:116
Page:1207-1215
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ISSN:0001-9240
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Container-title:The Aeronautical Journal
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language:en
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Short-container-title:Aeronaut. j.
Author:
Punniyakotti S.,Stollery J. L.
Abstract
Abstract
Existing theories are reviewed and compared. From the Tangent Wedge formula a simple expression for the normal force on thin wings is derived and compared with some existing experimental data, which cover the whole supersonic-hypersonic range of Mach numbers.
Publisher
Cambridge University Press (CUP)
Subject
Aerospace Engineering