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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

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

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

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Publish Date

1989

Publisher

Cranfield Institute of Technology, College of Aeronautics

Language

-

Pages

-

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