Find the wave drag of an (8 %) thick biconvex airfoil at free stream Mach number of
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Find the wave drag of an \(8 \%\) thick biconvex airfoil at free stream Mach number of \(\mathrm{M}=2\).
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Related Book For
Fundamentals Of Modern Unsteady Aerodynamics
ISBN: 9783030607760,9783030607777
3rd Edition
Authors: Ülgen Gülçat
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