Publication Date:
2019-07-13
Description:
It is proposed to solve the exact transonic potential flow equation on a mesh constructed from small volume elements, which can be conveniently packed around any reasonably smooth configuration. The calculation is performed on two sets of interlocking cells. The velocity and density are calculated in the primary cells, and a flux balance is then established in the secondary cells. The scheme is desymmetrized by the addition of artificial viscosity in the supersonic zone. Some results are included for a swept wing and a wing-cylinder combination.
Keywords:
AERODYNAMICS
Type:
AIAA PAPER 77-635
,
Computational Fluid Dynamics Conference; Jun 27, 1977 - Jun 28, 1977; Albuquerque, NM
Format:
text