Computation of field structure and aerodynamic characteristics of delta wings at high angles of attack

DOI10.1007/BF02465431zbMath1144.76318MaRDI QIDQ939949

Li-Zhi Yang, Zheng-Hong Gao

Publication date: 1 September 2008

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

zbMATH Keywords

computational methodvortex flowhigh angle of attack

Mathematics Subject Classification ID

Finite volume methods applied to problems in fluid mechanics (76M12) General aerodynamics and subsonic flows (76G25)

Related Items (1)

Sharp maximal inequalities for stochastic processes

Cites Work

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

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