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A three-dimensional moving mesh method for the calculation of unsteady transonic flows

Published online by Cambridge University Press:  04 July 2016

A. L. Gaitonde  and
S. P. Fiddes
A. L. Gaitonde
Affiliation:
Department of Aerospace EngineeringUniversity of Bristol, Bristol, United Kingdom
S. P. Fiddes
Affiliation:
Department of Aerospace EngineeringUniversity of Bristol, Bristol, United Kingdom
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Abstract

A three-dimensional moving mesh method for solving the Euler equations describing the compressible flow about a wing undergoing arbitrary motions and deformations is described. A finite-volume formulation is chosen where the volumes distort as the wing moves or deforms. By using transfinite interpolation, a technique for generating the required sequence of grids has been developed. Furthermore, as the speeds of the grid at the vertices of the finite volumes are required by the flow solver, transfinite interpolation is also used to obtain these by interpolation of the boundary speeds. A two-dimensional version of the method has also been developed and results for both two- and three-dimensional transonic flows are presented and compared with experimental data where available.

Type
Research Article
Information
The Aeronautical Journal , Volume 99 , Issue 984 , April 1995 , pp. 150 - 160
Copyright
Copyright © Royal Aeronautical Society 1995 

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