Research on the hysteresis properties of unsteady aerodynamics about the oscillating wings

DOI10.1007/BF02452488zbMath0954.76035MaRDI QIDQ1818202

Zheng-Hong Gao

Publication date: 8 February 2001

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

zbMATH Keywords

hysteresisunsteady aerodynamicsdelta wingangles of attackrectangular wingimplicit residual smoothingfour-stage Runge-Kutta time-stepping schemelocal variable parameterspitching oscillating wings

Mathematics Subject Classification ID

Finite difference methods applied to problems in fluid mechanics (76M20) General aerodynamics and subsonic flows (76G25) Gas dynamics (general theory) (76N15)

Cites Work

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

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