@inproceedings{e7f27f9745774f0db447c90c9ead60b1,
title = "Application of BCFD unstructured grid solver to simulation of micro-ramp control of shock/boundary layer interactions",
abstract = "An unstructured grid solver implemented in the BCFD code has been applied to simulate the effect of a micro-ramp on oblique shock wave/boundary layer interactions. Specifically, the micro-ramp's ability to prevent inlet unstart was examined. The 3D Reynolds-averaged Navier-Stokes equations were solved by an implicit time-marching method. Starting from a steady-state solution at a freestream Mach number of 2.0, the upstream boundary condition was perturbed to simulate a disturbance upstream of the oblique shock wave/boundary layer interaction. The reaction of the flow field to this disturbance was examined for cases with and without a micro-ramp. The results are in agreement with the previous findings of Anderson et al.",
author = "Shinn, {A. F.} and Vanka, {S. P.} and M. Mani and A. Dorgan and T. Michal",
year = "2007",
doi = "10.2514/6.2007-3914",
language = "English (US)",
isbn = "1563478986",
series = "Collection of Technical Papers - AIAA Applied Aerodynamics Conference",
publisher = "American Institute of Aeronautics and Astronautics Inc.",
pages = "315--326",
booktitle = "Collection of Technical Papers - 25th AIAA Applied Aerodynamics Conference, 2007",
note = "25th AIAA Applied Aerodynamics Conference, 2007 ; Conference date: 25-06-2007 Through 28-06-2007",
}