TOWARD A UNIFIED LIFT MODEL FOR USE IN ROTOR BLADE STABILITY ANALYSES.

  • David A. Peters

Research output: Contribution to journalArticlepeer-review

84 Scopus citations
Original languageEnglish
Pages (from-to)32-42
Number of pages11
JournalJournal of the American Helicopter Society
Volume30
Issue number3
DOIs
StatePublished - 1985

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