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Study and application of calculation method for adjusting the matching parameters of turbine nozzle area and engine nozzle radius

Research output: Contribution to journalArticlepeer-review

Original languageEnglish
Pages (from-to)145
Number of pages1
JournalHangkong Dongli Xuebao/Journal of Aerospace Power
Volume17
Issue number2
StatePublished - Apr 2002

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