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

Date

1989-08

Authors

Llewelyn-Davies, D. I. T. P.

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Cranfield Institute of Technology; College of Aeronautics

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Technical Report

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Free to read from

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Github

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