Author: He J-H.
Source: Aircraft Engineering and Aerospace Technology: An International Journal, Volume 74, Number 1, 2002 , pp. 9-11(3)
Publisher: Emerald Group Publishing Limited
Abstract:
By the semi-inverse method proposed by He, a variational principle is established for steady flow over a thin, symmetric, non-lifting aerofoil. The nonlinear, small-disturbance, velocity-potential equation is obtained by minimizing the obtained functional, and all boundary conditions are converted into natural boundary conditions, resulting in much convenience when incorporating the finite element method.Keywords: Flow; Finite Element Method
Document Type: Research article
DOI: 10.1108/00022660210414976
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