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DTIC ADA182801: Alternative Method of Calculation of Effective Wake... |
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by Defense Technical Information Center |
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The partial differential equation for the perturbed |
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pressure field of a propulsor operating in a non uniform |
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flow was transformed into a simple form due to Goodman. |
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Starting from the available solution for a flow with no |
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shear, an iterative procedure was selected to derive a |
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numerical solution for shear flow. The equivalent |
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integral equation based on solving Laplace's equation |
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would involve the numerical calculation of a five fold |
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integral over an infinite computational domain for each |
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interation. Keywords: Hydrodynamics; Shear flow; |
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Propulsion. |
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Date Published: 2018-02-15 04:37:20 |
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Identifier: DTIC_ADA182801 |
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Item Size: 67218264 |
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Language: english |
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Media Type: texts |
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# Topics |
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DTIC Archive; McKee,Glenn; STEVENS IN... |
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