What should be the minimum value of reduced frequency (mathrm{k}) for a thin airfoil in a free
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What should be the minimum value of reduced frequency \(\mathrm{k}\) for a thin airfoil in a free stream Mach number of 6 so that the piston theory is valid?
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Related Book For
Fundamentals Of Modern Unsteady Aerodynamics
ISBN: 9783030607760,9783030607777
3rd Edition
Authors: Ülgen Gülçat
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