The calculation of the profile drag of aerofoils and bodies of revolution at supersonic speeds

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dc.creator Young, A. D.
dc.date 2012-09-12T14:40:00Z
dc.date 2012-09-12T14:40:00Z
dc.date 1953-04
dc.date.accessioned 2022-05-09T10:17:21Z
dc.date.available 2022-05-09T10:17:21Z
dc.identifier http://dspace.lib.cranfield.ac.uk/handle/1826/7571
dc.identifier.uri https://reports.aerade.cranfield.ac.uk/handle/1826.2/4750
dc.description The effects of viscosity on the aerodynamic characteristics of wings and bodies at supersonic speeds can be assessed if we can calculate… Continues...
dc.language en
dc.publisher College of Aeronautics, Cranfield
dc.relation College Reports
dc.relation 73
dc.title The calculation of the profile drag of aerofoils and bodies of revolution at supersonic speeds
dc.type Report


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