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Computational study of shock control at transonic speed
No description available.
Links & Downloads
http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.323930
Tags
629.1323
Flow; Aerofoils
Additional Fields
Identifer
oai:union.ndltd.org:bl.uk/oai:ethos.bl.uk:323930
Date
January 2000
Creators
Zhu, Yu Ping
Publisher
Cranfield University
Source Sets
Ethos UK
Detected Language
English
Type
Electronic Thesis or Dissertation
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