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- W1995758049 abstract "Non-unique numerical solutions of transonic flows over airfoils have been found, first for potential flow equation, and later for Euler and RANS equations. The studies have also been extended to unsteady flow simulations, and non-unique numerical solutions continue to be demonstrated. The question of whether three-dimensional effect can have a further influence on the uniqueness of the transonic flow solution remain an important one. Hitherto wings supporting non-unique solutions in transonic solutions have not been studied. Research in this direction will further our understanding of the behavior of non-unique transonic flows. This paper studied a set of four wings based on recently designed symmetrical airfoils that have been found to support non-unique transonic solutions in both steady and unsteady flows in a narrow band of transonic Mach numbers. The aspect ratios of the wings have been varied as a way to control the extend of the three-dimensional effect. For certain of these airfoils, the non-unique solutions cease to exist when extended to a full wing, while for others, non-unique solutions continue to exist depending on the choice of the aspect ratios of the wings. The flow conditions that support non-unique solutions also tend to change when the airfoils are extended to wings of different aspect ratios. The scope of the study is, at present, limited to Euler solutions." @default.
- W1995758049 created "2016-06-24" @default.
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- W1995758049 date "2014-06-13" @default.
- W1995758049 modified "2023-09-28" @default.
- W1995758049 title "Studies of Wings Supporting Non-unique Solutions in Transonic Flows" @default.
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- W1995758049 doi "https://doi.org/10.2514/6.2014-2928" @default.
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