A New Approach of Using Porous Bleed Boundary Conditions - Application of Local Porosity
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Publisher
Springer Nature Switzerland
Link
https://link.springer.com/content/pdf/10.1007/978-3-031-40482-5_34
Reference12 articles.
1. Abrahamson, K., Brower, D.: An empirical boundary condition for numerical simulation of porous plate bleed flows. In: 26th Aerospace Sciences Meeting Reston, Virigina: American Institute of Aeronautics and Astronautics (1988)
2. Chyu, W.J., Howe, G.W., Shih, T.I.-P.: Bleed-boundary conditions for numerically simulated mixed-compression supersonic inlet flow. J. Propuls. Power 8(4), 862–868 (1992)
3. Paynter, G.C., Treiber, D.A., Kneeling, W.D.: Modeling supersonic inlet boundary-layer bleed roughness. J. Propuls. Power 9(4), 622–627 (1993)
4. Slater, J.W.: Improvements in modeling 90-degree bleed holes for supersonic inlets. J. Propuls. Power 28(4), 773–781 (2012)
5. Choe, Y., Kim, C., Kim, K.: Effects of optimized bleed system on supersonic inlet performance and buzz. J. Propuls. Power 36(2), 211–222 (2020)
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1. Experimental and numerical investigation of porous bleed control for supersonic/subsonic flows, and shock-wave/boundary-layer interactions;Aerospace Science and Technology;2024-04
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