Transform the spanwise (mathrm{y}, eta) coordinates into (phi, theta), and obtain Eq. 4.21 as Glauert did. Eq.
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Transform the spanwise \(\mathrm{y}, \eta\) coordinates into \(\phi, \theta\), and obtain Eq. 4.21 as Glauert did.
Eq. 4.21
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Related Book For
Fundamentals Of Modern Unsteady Aerodynamics
ISBN: 9783030607760,9783030607777
3rd Edition
Authors: Ülgen Gülçat
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