| 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 | 45 | 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 | 32 | 2018 |
| Investigation of a Cylinder-Induced Transitional Shock Wave-Boundary Layer Interaction using Laser Diagnostics CS Combs, EL Lash, JD Schmisseur 32nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference, 4321, 2016 | 31 | 2016 |
| 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 |
| 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 |
| Unsteady Extinction of Opposed Jet Ethylene/Methane HiFIRE Surrogate Fuel Mixtures vs. Air S Vaden, R Debes, EL Lash, R Burk, CM Boyd, L Wilson, G Pellett 45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 4883, 2009 | 14 | 2009 |
| Shockwave/boundary-layer interaction studies performed in the NASA Langley 20-Inch Mach 6 Air Tunnel BF Bathel, SB Jones, AN Watkins, S Berry, K Goodman, CS Combs, ... AIAA Aviation 2019 Forum, 2904, 2019 | 9 | 2019 |
| Dynamic Mode Decomposition of Unsteady Pressure-Sensitive Paint Measurements for the NASA Unitary Plan Wind Tunnel Tests J Li, EL Lash, N Roozeboom, TJ Garbeff, C Henze, D Murakami, N Smith, ... AIAA SCITECH 2022 Forum, 0141, 2022 | 7 | 2022 |
| NASA’s unsteady pressure-sensitive paint research and operational capability developments N Roozeboom, DD Murakami, J Li, M Shaw-Lecerf, EL Lash, N Califano, ... AIAA SCITECH 2023 Forum, 0636, 2023 | 6 | 2023 |
| Exploration of upstream influence and the role of shock generator geometry in shock wave/transitional boundary layer interactions at Mach 1.8 edge conditions EL Lash, M Gragston, Z McDaniel, PA Kreth, JD Schmisseur AIAA Aviation 2020 Forum, 2999, 2020 | 6 | 2020 |
| Trajectory analysis and comparison of a linear aerospike nozzle to a conventional bell nozzle for SSTO flight EL Lash | 6 | 2015 |
| Preliminary Unsteady Characterization of Shock Wave/Boundary Layer Interactions on a 4% Scale SLS Model using uPSP and Shadowgraph EL Lash, N Roozeboom, JK Baerny, TJ Garbeff AIAA AVIATION 2020 FORUM, 2725, 2020 | 5 | 2020 |
| Implementation of the Lifetime Method in Unsteady Pressure-Sensitive Paint Measurements DD Murakami, M Shaw-Lecerf, EL Lash, K Lyons, N Roozeboom AIAA SCITECH 2023 Forum, 0635, 2023 | 4 | 2023 |
| Methodology for Validation of Unsteady Pressure-Sensitive Paint Measurements using Pressure Transducers M Shaw-Lecerf, EL Lash, DD Murakami, N Roozeboom, J Li, PG Bremner AIAA SCITECH 2023 Forum, 0639, 2023 | 4 | 2023 |
| Assessment of aerospike nozzle for single-stage to orbit flight EL Lash, TM Moeller 51st AIAA/SAE/ASEE Joint Propulsion Conference, 3979, 2015 | 3 | 2015 |
| NASA's Unsteady Pressure-Sensitive Paint Phase I Development Overview EL Lash, N Roozeboom, DD Murakami, M Shaw-Lecerf, J Li, N Califano, ... AIAA SCITECH 2024 Forum, 0880, 2024 | 2 | 2024 |
| Infrared Reflection Removal in Wind Tunnels using Polarization Theory N Califano, EL Lash, TJ Garbeff, N Roozeboom AIAA SCITECH 2023 Forum, 0638, 2023 | 2 | 2023 |
| Joint Acceptance Attenuation Factor of Integrated Pressure with Unsteady Pressure-Sensitive Paint Measurements J Li, M Shaw-Lecerf, DD Murakami, EL Lash, N Roozeboom, PG Bremner AIAA SCITECH 2023 Forum, 0637, 2023 | 2 | 2023 |
| Characterizing the Unsteady Dynamics of Cylinder-Induced Shock Wave/Transitional Boundary Layer Interactions Using Non-Intrusive Diagnostics EL Lash | 2 | 2020 |
John SchmisseurProfessor of Aerospace Engineering, University of TennesseeDirección de correo verificada de utsi.edu
