Equations of Perturbation Growth in Aircraft Wakes |
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| Authors: | A M Gaifullin |
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| Institution: | (1) Department of Mechanical Engineering, Imperial College London, Exhibition Road, London, SW7 2BX, UK; |
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| Abstract: | Equations for the perturbation amplitude in the vortex wake of an aircraft with a high-aspect-ratio wing are derived. The effect of the perturbing factor frequency, the proximity of the ground, and the turbulent atmosphere characteristics on the wake evolution is investigated. |
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