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.
URI:
http://dspace.lib.cranfield.ac.uk/handle/1826/7571
Date:
1953-04
Abstract:
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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[280]
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