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pro vyhledávání: '"Axdahl, Erik L"'
Autor:
Axdahl, Erik Lee
One of the current goals of research in hypersonic, airbreathing propulsion is access to higher Mach numbers. A strong driver of this goal is the desire to integrate a scramjet engine into a transatmospheric vehicle airframe in order to improve perfo
Externí odkaz:
http://hdl.handle.net/1853/50290
