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Showing results 1 to 6 of 6

1
Effect of Mach Number on Flow Past Microramps

Lee, S.; Loth, E.; Georgiadis, N. J.; DeBonis, J. R., AIAA JOURNAL, v.49, no.1, pp.97 - 110, 2011-01

2
Impact of Ramped Vanes on Normal Shock Boundary-Layer Interaction

Lee, S.; Loth, E., AIAA JOURNAL, v.50, no.10, pp.2069 - 2079, 2012-10

3
Microramps Upstream of an Oblique-Shock/Boundary-Layer Interaction

Lee, S.; Goettke, M. K.; Loth, E.; Tinapple, J.; Benek, John, AIAA JOURNAL, v.48, no.1, pp.104 - 118, 2010-01

4
Normal shock boundary layer control with various vortex generator geometries

Lee, S.; Loth, E.; Babinsky, H., COMPUTERS & FLUIDS, v.49, no.1, pp.233 - 246, 2011-10

5
On ramped vanes to control normal shock boundary layer interactions

Lee, S.; Loth, E., AERONAUTICAL JOURNAL, v.122, no.1256, pp.1568 - 1585, 2018-10

6
Supersonic boundary-layer interactions with various micro-vortex generator geometries

Lee, S.; Loth, E., AERONAUTICAL JOURNAL, v.113, no.1149, pp.683 - 697, 2009-11

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