Proposed inflow/outflow boundary condition for direct computation of aerodynamic sound

Research output: Contribution to journalArticlepeer-review

Original languageEnglish (US)
Pages (from-to)740-742
Number of pages3
JournalAIAA journal
Volume35
Issue number4
DOIs
StatePublished - Jan 1 1997
Externally publishedYes

ASJC Scopus subject areas

  • Aerospace Engineering

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