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pro vyhledávání: '"thrust coefficient efficiency loss"'
Publikováno v:
宇宙輸送シンポジウム 平成15年度 = Proceedings of Space Transportation Symposium FY2003. :139-142
In the present study were examined numerically and experimentally the off-design performance characteristics on an axisymmetric plug nozzle with variable throat area. In this nozzle concept its throat area can be changed by translating the plug in th