Abstract
The problem of determining the optimal contour of a two-dimensional jet engine outlet system was solved in [1] using the direct method of the calculus of variations. In this study the method is developed for designing the optimal contour of a three-dimensional outlet system providing maximum thrust in a given direction.
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REFERENCES
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Aukin, M.K., Tagirov, R.K. Determining the Optimal Contour of a Three-Dimensional Supersonic Jet Engine Outlet System. Fluid Dynamics 38, 143–152 (2003). https://doi.org/10.1023/A:1023355516180
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DOI: https://doi.org/10.1023/A:1023355516180