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INVESTIGATION OF THE EFFECTS OF NON-UNIFORM THROAT FLOW ON BASE PRESSURE AT SUPERSONIC FLIGHT SPEEDS.

Research output: Contribution to journalConference articlepeer-review

Original languageEnglish (US)
JournalAIAA Paper
DOIs
StatePublished - 1984
Externally publishedYes

ASJC Scopus subject areas

  • General Engineering

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