Publication Date:
2013-08-31
Description:
An explicit multistage Runge-Kutta type of time-stepping scheme is used for solving transonic flow past a transport type wing/fuselage configuration. Solutions for both Euler and Navier-Stokes equations are obtained for quantitative assessment of boundary layer interaction effects. The viscous solutions are obtained on both a medium resolution grid of approximately 270,000 points and a find grid of 460,000 points to assess the effects of grid density on the solution. Computed pressure distributions are compared with the experimental data.
Keywords:
FLUID MECHANICS AND HEAT TRANSFER
Type:
Transonic Symposium: Theory, Application, and Experiment, Volume 1, Part 2; p 571-579
Format:
application/pdf
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