| Experimental study of the mean structure and quasi-conical scaling of a swept-compression-ramp interaction at Mach 2 L Vanstone, MN Musta, S Seckin, N Clemens Journal of Fluid Mechanics 841, 1-27, 2018 | 52 | 2018 |
| Proper orthogonal decomposition analysis of swept-ramp shock-wave/boundary-layer unsteadiness at Mach 2 L Vanstone, NT Clemens AIAA Journal 57 (8), 3395-3409, 2019 | 31 | 2019 |
| Effect of shock-wave boundary layer interaction on vibratory response of compliant panel MA Eitner, YJ Ahn, L Vanstone, MN Musta, J Sirohi, N Clemens AIAA Aviation 2021 Forum, 2493, 2021 | 28 | 2021 |
| Closed-loop control of shock-train location in a combusting scramjet L Vanstone, KE Hashemi, J Lingren, MR Akella, NT Clemens, J Donbar, ... Journal of Propulsion and Power 34 (3), 660-667, 2018 | 28 | 2018 |
| Micro vortex generator control of axisymmetric high-speed laminar boundary layer separation D Estruch-Samper, L Vanstone, R Hillier, B Ganapathisubramani Shock Waves 25, 521-533, 2015 | 27 | 2015 |
| Simple physics-based model for the prediction of shock-train location L Vanstone, J Lingren, NT Clemens Journal of Propulsion and Power 34 (6), 1428-1441, 2018 | 21 | 2018 |
| Investigation of flow-structure coupling for a compliant panel under a shock/boundary-layer interaction using fast-response PSP MN Musta, L Vanstone, YJ Ahn, M Eitner, J Sirohi, N Clemens AIAA Aviation 2021 Forum, 2809, 2021 | 20 | 2021 |
| Role of boundary-layer on unsteadiness on a Mach 2 swept-ramp shock/boundary-layer interaction using 50 kHz PIV L Vanstone, M Saleem, S Seckin, NT Clemens 55th AIAA Aerospace Sciences Meeting, 0757, 2017 | 19 | 2017 |
| Modal parameter estimation of a compliant panel using phase-based motion magnification and stereoscopic digital image correlation M Eitner, M Musta, L Vanstone, J Sirohi, N Clemens Experimental Techniques 45, 287-296, 2021 | 18 | 2021 |
| Shock induced separation in transitional hypersonic boundary layers L Vanstone, D Estruch-Samper, R Hillier, B Ganapathisubramani 43rd AIAA Fluid Dynamics Conference, 2736, 2013 | 16 | 2013 |
| Toluene-based planar laser-induced fluorescence imaging of temperature in hypersonic flows D Estruch-Samper, L Vanstone, R Hillier, B Ganapathisubramani Experiments in Fluids 56, 1-13, 2015 | 15 | 2015 |
| Axisymmetric flare-induced separation of high-speed transitional boundary layers D Estruch-Samper, B Ganapathisubramani, L Vanstone, R Hillier 50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and …, 2012 | 15 | 2012 |
| Unsteadiness mechanisms of a swept compression-ramp shock/boundary layer interaction at Mach 2 L Vanstone, NT Clemens AIAA Scitech 2019 Forum, 0095, 2019 | 14 | 2019 |
| Effect of upstream boundary layer on unsteadiness of swept-ramp shock/boundary layer interactions at Mach 2 L Vanstone, M Saleem, S Seckin, NT Clemens 54th AIAA Aerospace Sciences Meeting, 0076, 2016 | 14 | 2016 |
| Closed-loop control of unstart in a Mach 1.8 isolator L Vanstone, A Bosco, Y Saleh, M Akella, NT Clemens, S Gogineni Journal of Propulsion and Power 36 (1), 153-157, 2020 | 13 | 2020 |
| Spectral Proper Orthogonal Decomposition Analysis of Shock-Wave/Boundary-Layer Interactions S Cottier, CS Combs, L Vanstone AIAA Aviation 2019 Forum, 3331, 2019 | 13 | 2019 |
| POD analysis of unsteadiness mechanisms within a swept compression-ramp shock-wave boundary-layer interaction at Mach 2 L Vanstone, S Seckin, NT Clemens 2018 AIAA Aerospace Sciences Meeting, 2073, 2018 | 13 | 2018 |
| Investigation of unsteadiness in a Mach 2 swept-ramp shock/boundary-layer interaction using 50 kHz PIV L Vanstone, M Nail Musta, NT Clemens, M Saleem, S Seckin 46th AIAA Fluid Dynamics Conference, 3338, 2016 | 13 | 2016 |
| Separated flow unsteadiness in a Mach 2 swept compression-ramp interaction using high-speed PSP L Vanstone, T Goller, L Mears, NT Clemens AIAA Aviation 2019 Forum, 3647, 2019 | 12 | 2019 |
| Experimental investigation of unsteadiness of swept-ramp shock/boundary layer interactions at Mach 2 L Vanstone, M Saleem, S Seckin, NT Clemens 45th AIAA Fluid Dynamics Conference, 2932, 2015 | 11 | 2015 |
