Compare the surface pressure coefficient obtained with Dowell method using (x_{0}=mathrm{b}) as expansion point and (e_{0}=0.12) and
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Compare the surface pressure coefficient obtained with Dowell method using \(x_{0}=\mathrm{b}\) as expansion point and \(e_{0}=0.12\) and \(f_{0}=2.4 / b\) with the pressure coefficient obtained using Stahara-Spreiter method for the \(6 \%\) thick Guderly airfoil. Discuss the choice of \(x_{0}=b\).
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Related Book For
Fundamentals Of Modern Unsteady Aerodynamics
ISBN: 9783030607760,9783030607777
3rd Edition
Authors: Ülgen Gülçat
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