The calculation of the profile drag of aerofoils and bodies of revolution at supersonic speeds
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The calculation of the profile drag of aerofoils and bodies of revolution at supersonic speeds
Young, A. D.
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https://reports.aerade.cranfield.ac.uk/handle/1826.2/4750
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The effects of viscosity on the aerodynamic characteristics of wings and bodies at supersonic speeds can be assessed if we can calculate… Continues...
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CoA. Reports
[280]
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