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Hypersonic curved compression inlet and its inverse design

This book presents systematic research results on curved shock wave-curved compression surface applied to the compression surface design of supersonic–hypersonic inlet, which is a brand new inlet design. The concept of supersonic inlet curved compression discussed originated from the author’s resear...

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Detalles Bibliográficos
Autor principal: Zhang, Kunyuan
Lenguaje:eng
Publicado: Springer 2020
Materias:
Acceso en línea:https://dx.doi.org/10.1007/978-981-15-0727-4
http://cds.cern.ch/record/2708793