Find the heat transfer rate (mathrm{q}_{mathrm{w}}) at (mathrm{x}=10 mathrm{~cm}) and (100 mathrm{~cm}) for the flat plate given
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Find the heat transfer rate \(\mathrm{q}_{\mathrm{w}}\) at \(\mathrm{x}=10 \mathrm{~cm}\) and \(100 \mathrm{~cm}\) for the flat plate given in Problem 7.31.
Problem 7.31
A flat plate of \(4 \mathrm{~m}\) long has the wall temperature of \(1200 \mathrm{~K}\) at zero angle of attack at free stream Mach number of 25 and \(85 \mathrm{~km}\) altitude. Using the data given obtain the pressure variation along the plate.
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Related Book For
Fundamentals Of Modern Unsteady Aerodynamics
ISBN: 9783030607760,9783030607777
3rd Edition
Authors: Ülgen Gülçat
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