Publication Date:
2019-07-13
Description:
A new boundary condition is presented.for simulating the flow over passively porous surfaces. The model builds on the prior work of R.H. Bush to eliminate the need for constructing grid within an underlying plenum, thereby simplifying the numerical modeling of passively porous flow control systems and reducing computation cost. Code experts.for two structured-grid.flow solvers, TLNS3D and CFL3D. and one unstructured solver, USM3Dns, collaborated with an experimental porosity expert to develop the model and implement it into their respective codes. Results presented,for the three codes on a slender forebody with circumferential porosity and a wing with leading-edge porosity demonstrate a good agreement with experimental data and a remarkable ability to predict the aggregate aerodynamic effects of surface porosity with a simple boundary condition.
Keywords:
Fluid Mechanics and Thermodynamics
Type:
AIAA Paper 2001-2412
,
19th Applied Aerodynamics Conference; Jun 11, 2001 - Jun 14, 2001; Anaheim, CA; United States
Format:
application/pdf
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