Numerical solution of the unsteady Euler equations for airfoils using approximate boundary conditions
Author:
Publisher
Springer Science and Business Media LLC
Subject
Mechanical Engineering,Computational Mechanics
Link
http://link.springer.com/content/pdf/10.1007/BF02484577.pdf
Reference10 articles.
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3. Jameson A, Schmidt W, Turkel E. Numerical solutions of the Euler equations by finite volume methods using Runge-Kutta time-stepping schemes. AIAA Paper 81-1259, June, 1981
4. Liu F, Cai J, Zhu Y, et al. Calculation of wing flutter by a coupled fluid-structure method.Journal of Aircraft, 2001, 38(2): 334–342
5. Tsai HM, Wong ASF, Cai J, et al. Unsteady flow calculations with a multi-block moving mesh algorithm.AIAA Journal, 2001, 39(6): 1021–1029
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