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DTIC ADA064311: Studies on Three-Dimensional Boundary Layers on Bod... |
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by Defense Technical Information Center |
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The laminar boundary-layer development near the nose of a |
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body of revolution and a two-dimensional airfoil is |
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investigated until the onset of leading-edge separation. |
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This is accomplished through the use of a coordinate |
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transformation which eliminates any geometrical |
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singularity at the nose in the governing boundary-layer |
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equations. The resulting equations are examined by both |
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asymptotic and numerical means. Comparable cases for the |
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three-dimensional body of revolution and the two- |
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dimensional airfoil are given and similarities as well as |
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differences are discussed. (Author) |
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Date Published: 2017-08-31 08:50:16 |
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Identifier: DTIC_ADA064311 |
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Item Size: 33213144 |
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Language: english |
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Media Type: texts |
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# Topics |
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DTIC Archive; Cebeci,Tuncer; DOUGLAS ... |
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