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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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COA_8909.PDF (5.73 MB)

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1989-08

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Cranfield Institute of Technology; College of Aeronautics

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Technical Report

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http://hdl.handle.net/1826/1084

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