Unconditional stable solutions of the Euler equations for two- and three-dimensional wings in arbitrary motion

DOI10.1007/BF02466991zbMath0844.76071MaRDI QIDQ1910322

Zheng-Hong Gao

Publication date: 1 April 1996

Published in: Applied Mathematics and Mechanics. (English Edition) (Search for Journal in Brave)

zbMATH Keywords

implicit residual smoothingfinite volume Euler methodrectangle wingsrigid and flexible pitching oscillationsRunge-Kutta time stepping scheme

Mathematics Subject Classification ID

Transonic flows (76H05) Existence, uniqueness, and regularity theory for compressible fluids and gas dynamics (76N10)

Related Items (2)

Computation of field structure and aerodynamic characteristics of delta wings at high angles of attack ⋮ Research on the hysteresis properties of unsteady aerodynamics about the oscillating wings

Cites Work

• Three-dimensional calculation of transonic viscous flows by an implicit method

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