| Investigating unsteady dynamics of cylinder-induced shock-wave/transitional boundary-layer interactions CS Combs, EL Lash, PA Kreth, JD Schmisseur AIAA journal 56 (4), 1588-1599, 2018 | 47 | 2018 |
| Image-based analysis of shock-wave/boundary-layer interaction unsteadiness CS Combs, PA Kreth, JD Schmisseur, EL Lash AIAA journal 56 (3), 1288-1293, 2018 | 33 | 2018 |
| Design and initial characterization of the UTSI Mach 4 Ludwieg tube PA Kreth, M Gragston, K Davenport, JD Schmisseur AIAA Scitech 2021 Forum, 0384, 2021 | 30 | 2021 |
| Developing an Image-Based Analysis of the Dynamics of Transitional Shock Wave-Boundary Layer Interactions EL Lash, CS Combs, PA Kreth, EA Beckman, JD Schmisseur 32nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference, 4320, 2016 | 27 | 2016 |
| Measurement of supersonic jet screech with focused laser differential interferometry TJ Price, M Gragston, JD Schmisseur, PA Kreth Applied Optics 59 (28), 8902-8908, 2020 | 25 | 2020 |
| Study of the dynamics of transitional shock wave-boundary layer interactions using optical diagnostics EL Lash, CS Combs, PA Kreth, JD Schmisseur 47th AIAA Fluid Dynamics Conference, 3123, 2017 | 25 | 2017 |
| Experimental investigation of a cylinder-induced transitional shock wave-boundary layer interaction EL Lash, CS Combs, PA Kreth, JD Schmisseur 55th AIAA Aerospace Sciences Meeting, 0760, 2017 | 24 | 2017 |
| Laser differential interferometry and schlieren as an approach to characterizing freestream disturbance levels AJ Harris, PA Kreth, CS Combs, JD Schmisseur 2018 AIAA Aerospace Sciences Meeting, 1100, 2018 | 22 | 2018 |
| Modal analysis of cylinder-induced transitional shock-wave/boundary-layer interaction unsteadiness ENA Hoffman, JM Rodriguez, SM Cottier, CS Combs, BF Bathel, ... AIAA journal 60 (5), 2730-2748, 2022 | 20 | 2022 |
| Numerical simulations of a cylinder-induced shock wave/boundary layer interaction SA Lindörfer, CS Combs, PA Kreth, JD Schmisseur 55th AIAA Aerospace Sciences Meeting, 0534, 2017 | 19 | 2017 |
| Characterization of Temperature Sensitive Paint for Application in Hypersonic Ludwieg Tubes at the University of Tennessee C Smith, PA Kreth, JD Schmisseur, G Strickland AIAA SCITECH 2022 Forum, 1660, 2022 | 17 | 2022 |
| Using high-frequency pulsed supersonic microjets to control resonant high-speed cavity flows PA Kreth, FS Alvi AIAA Journal 58 (8), 3378-3392, 2020 | 16 | 2020 |
| Microjet based active flow control on a fixed wing UAV P Kreth, F Alvi, V Kumar, R Kumar 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and …, 2010 | 16 | 2010 |
| Scaling of cylinder-generated shock-wave/turbulent boundary-layer interactions SA Lindörfer, CS Combs, PA Kreth, RB Bond, JD Schmisseur Shock Waves 30 (4), 395-407, 2020 | 14 | 2020 |
| Characterizing the streamwise development of surface roughness effects on a supersonic boundary layer BD Kocher, CS Combs, PA Kreth, JD Schmisseur 2018 Fluid Dynamics Conference, 4047, 2018 | 13 | 2018 |
| Velocity field measurements on high-frequency, supersonic microactuators PA Kreth, MY Ali, EJ Fernandez, FS Alvi Experiments in Fluids 57, 1-13, 2016 | 13 | 2016 |
| Investigation of the effects of distributed surface roughness on supersonic flows BD Kocher, CS Combs, PA Kreth, JD Schmisseur, SJ Peltier 47th AIAA Fluid Dynamics Conference, 4313, 2017 | 11* | 2017 |
| An Investigation of the Role of an Upstream Burst Diaphragm on Flow Quality within a Ludwieg tube using RANS SA Lindörfer, P Anusonti-Inthra, CS Combs, PA Kreth, JD Schmisseur 46th AIAA Fluid Dynamics Conference, 3801, 2016 | 10 | 2016 |
| Design and Initial Characterization of the UTSI Mach 7 Ludwieg Tube M Gragston, K Davenport, F Siddiqui, N Webber, CD Smith, PA Kreth, ... AIAA SCITECH 2023 Forum, 1457, 2023 | 9 | 2023 |
| Modal analysis of a Mach 1.5 underexpanded jet using time-resolved optical diagnostics TJ Price, M Gragston, PA Kreth AIAA Scitech 2020 Forum, 1069, 2020 | 9 | 2020 |
John SchmisseurProfessor of Aerospace Engineering, University of Tennessee在 utsi.edu 的电子邮件经过验证
