The choice of (cot (theta / 2)) for the chordwise variation of the pressure coefficient gives the
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The choice of \(\cot (\theta / 2)\) for the chordwise variation of the pressure coefficient gives the \(1 / \varepsilon^{1 / 2}\) type singularity at the leading edge and \(\varepsilon^{1 / 2}\) type distribution at the trailing edge.
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Related Book For
Fundamentals Of Modern Unsteady Aerodynamics
ISBN: 9783030607760,9783030607777
3rd Edition
Authors: Ülgen Gülçat
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