@article{funderburk_narayanaswamy_2019, title={Experimental Investigation of Microramp Control of an Axisymmetric Shock/Boundary-Layer Interaction}, volume={57}, ISSN={["1533-385X"]}, url={http://www.scopus.com/inward/record.url?eid=2-s2.0-85070370366&partnerID=MN8TOARS}, DOI={10.2514/1.J057846}, abstractNote={Mitigation of shock-induced boundary-layer separation using vortex generators (VGs) is an emerging flow control approach in planar inlet geometries. In the present work, an experimental campaign is...}, number={8}, journal={AIAA JOURNAL}, author={Funderburk, Morgan L. and Narayanaswamy, Venkateswaran}, year={2019}, month={Aug}, pages={3379–3394} }
 @article{funderburk_narayanaswamy_2019, title={Investigation of Negative Surface Curvature Effects in Axisymmetric Shock/Boundary-Layer Interaction}, volume={57}, ISSN={["1533-385X"]}, url={http://www.scopus.com/inward/record.url?eid=2-s2.0-85067429803&partnerID=MN8TOARS}, DOI={10.2514/1.J057275}, abstractNote={The shock/boundary-layer interactions (SBLIs) generated by a negatively curved compression ramp are investigated. The ramp was mounted to the inner surface of a semicircular hollow cylinder, along ...}, number={4}, journal={AIAA JOURNAL}, author={Funderburk, Morgan L. and Narayanaswamy, Venkateswaran}, year={2019}, month={Apr}, pages={1594–1607} }
 @article{funderburk_narayanaswamy_2019, title={Spectral signal quality of fast pressure sensitive paint measurements in turbulent shock-wave/boundary layer interactions}, volume={60}, ISSN={["1432-1114"]}, url={http://www.scopus.com/inward/record.url?eid=2-s2.0-85073063330&partnerID=MN8TOARS}, DOI={10.1007/s00348-019-2799-x}, number={10}, journal={EXPERIMENTS IN FLUIDS}, author={Funderburk, Morgan L. and Narayanaswamy, Venkateswaran}, year={2019}, month={Oct} }
 @article{funderburk_narayanaswamy_2016, title={Experimental investigation of primary and corner shock boundary layer interactions at mild back pressure ratios}, volume={28}, ISSN={["1089-7666"]}, url={http://www.scopus.com/inward/record.url?eid=2-s2.0-84983745346&partnerID=MN8TOARS}, DOI={10.1063/1.4960963}, abstractNote={Unstart of rectangular inlets occurs as a result of interactions between shock-induced separation units along the floor/ceiling, corner, and sidewalls. While a significant body of literature exists regarding the individual flow interactions at the inlet floor/ceiling (called primary separation) and sidewalls, limited efforts have focused on the mean and dynamic features of the corner separation. Experiments are conducted to investigate primary and corner shock boundary layer interactions (SBLI) with the objectives of elucidating the flow interactions that occur in the corner, and characterizing the interaction between the corner and primary separation units at mild back pressure ratios. Surface streakline flow visualization and high-frequency wall static pressure measurements are performed along the centerline and corner regions of shock-induced flow separation generated by a 12° compression ramp in a Mach 2.5 flow. Sidewall fences that extend upstream of the leading edge of the flat plate generate corner separation of adequate size to determine the mean flow structures, characterize the unsteady motions, and investigate the mechanisms that drive the unsteadiness of primary and corner SBLI. Results show that the corner and primary SBLI units differ fundamentally in both their mean and unsteady features and their response to upstream and downstream flow perturbations. These observations suggest that the two behave as independent units at this relatively low shock-induced back pressure ratio.}, number={8}, journal={PHYSICS OF FLUIDS}, author={Funderburk, M. and Narayanaswamy, V.}, year={2016}, month={Aug} }