VELOCITY-FIELD OF A LIFTING ROTOR BLADE IN HOVER

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dc.contributor.authorKOMERATH, NMko
dc.contributor.authorTHOMPSON, TLko
dc.contributor.authorKwon, Oh Joonko
dc.contributor.authorGRAY, RBko
dc.date.accessioned2009-07-30-
dc.date.available2009-07-30-
dc.date.created2012-02-06-
dc.date.created2012-02-06-
dc.date.issued1988-03-
dc.identifier.citationJOURNAL OF AIRCRAFT, v.25, no.3, pp.250 - 257-
dc.identifier.issn0021-8669-
dc.identifier.urihttp://hdl.handle.net/10203/10401-
dc.description.sponsorshipThe authors gratefully acknowledge the support of this work by the U.S. Army Research Office as part of the Center for Rotary Wing Aircraft Technology, Contract DAAG29-82-K- 0094, monitored by Dr. Robert E. Singleton.en
dc.languageEnglish-
dc.language.isoen_USen
dc.publisherAMER INST AERONAUT ASTRONAUT-
dc.titleVELOCITY-FIELD OF A LIFTING ROTOR BLADE IN HOVER-
dc.typeArticle-
dc.identifier.wosidA1988N844500010-
dc.identifier.scopusid2-s2.0-0023966438-
dc.type.rimsART-
dc.citation.volume25-
dc.citation.issue3-
dc.citation.beginningpage250-
dc.citation.endingpage257-
dc.citation.publicationnameJOURNAL OF AIRCRAFT-
dc.identifier.doi10.2514/3.45585-
dc.embargo.liftdate9999-12-31-
dc.embargo.terms9999-12-31-
dc.contributor.localauthorKwon, Oh Joon-
dc.contributor.nonIdAuthorKOMERATH, NM-
dc.contributor.nonIdAuthorTHOMPSON, TL-
dc.contributor.nonIdAuthorGRAY, RB-
dc.type.journalArticleArticle-
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