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.creator Llewelyn-Davies, D. I. T. P.
dc.date 2006-05-24T10:29:34Z
dc.date 2006-05-24T10:29:34Z
dc.date 1989-08
dc.date.accessioned 2022-05-09T10:17:12Z
dc.date.available 2022-05-09T10:17:12Z
dc.identifier 1 871564 01 8
dc.identifier http://hdl.handle.net/1826/1084
dc.identifier.uri https://reports.aerade.cranfield.ac.uk/handle/1826/1084
dc.format 6008119 bytes
dc.format application/pdf
dc.language en
dc.publisher Cranfield Institute of Technology; College of Aeronautics
dc.relation College of Aeronautics Reports
dc.relation CIT/CoA-8909
dc.title 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
dc.type Technical Report


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