The applications of computational fluid dynamics to problems in rotorcraft aerodynamics:

dc.contributor.authorShaw, Scotten_UK
dc.date1995en_UK
dc.date.accessioned2005-11-23T12:19:54Z
dc.date.available2005-11-23T12:19:54Z
dc.date.issued1995en_UK
dc.description.abstractThe flowfield around a helicopter rotor in forward flight is intrinsically unsteady and contains many complex interacting flow phenomena. As a consequence experimental investigations are difficult to perform, difficult to interpret and costly. There is a clear need for reliable computational methods whose uncertainties are less than those of experiment. In this paper computational methods currently available for the solution of problems in rotor aerodynamics are examined and the current direction of research in this field identified.en_UK
dc.description.sponsorshipThe Universityen_UK
dc.format.extent1963 bytes
dc.format.extent1965573 bytes
dc.format.mimetypetext/plain
dc.format.mimetypeapplication/pdf
dc.identifier.urihttp://hdl.handle.net/1826/187
dc.language.isoen_UKen_UK
dc.relation.ispartofseriesCollege of Aeronautics Report;9502en_UK
dc.relation.ispartofseriesCU/CoA/R;9502en_UK
dc.titleThe applications of computational fluid dynamics to problems in rotorcraft aerodynamics:en_UK
dc.typeTechnical Reporten_UK

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