The effect of pitch and yaw on the aerodynamic interference between two identical, unstaggered, axisymmetrical bodies whose centrelines are parallel and separated by 1.11 body diameters

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dc.contributor.authorLlewelyn-Davies, D. I. T. P.
dc.date.accessioned2006-05-24T10:29:34Z
dc.date.available2006-05-24T10:29:34Z
dc.date.issued1989-08
dc.format.extent6008119 bytes
dc.format.mimetypeapplication/pdf
dc.identifier.isbn1 871564 01 8
dc.identifier.urihttp://hdl.handle.net/1826/1084
dc.language.isoenen
dc.publisherCranfield Institute of Technology; College of Aeronauticsen
dc.relation.ispartofseriesCollege of Aeronautics Reportsen
dc.relation.ispartofseriesCIT/CoA-8909en
dc.titleThe effect of pitch and yaw on the aerodynamic interference between two identical, unstaggered, axisymmetrical bodies whose centrelines are parallel and separated by 1.11 body diametersen
dc.typeTechnical Reporten

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