| Year |
Citation |
Score |
| 2020 |
Bunnell S, Gorrell S, Salmon J, Thelin C, Ruoti C. Structural Design Space Exploration Using Principal Component Analysis Journal of Computing and Information Science in Engineering. 20. DOI: 10.1115/1.4047428 |
0.328 |
|
| 2020 |
Fernelius MH, Gorrell SE. Mapping Efficiency of a Pulsing Flow-Driven Turbine Journal of Fluids Engineering-Transactions of the Asme. 142. DOI: 10.1115/1.4045993 |
0.372 |
|
| 2016 |
Lundgreen RK, Oliphant KN, Maynes D, Gorrell SE. High suction performance pumps with large inlet blade angles and an integrated stability control device 52nd Aiaa/Sae/Asee Joint Propulsion Conference, 2016. |
0.428 |
|
| 2016 |
Peterson MW, Gorrell SE, List M, Custer C. Implementation of fourier methods in CFD to analyze distortion transfer and generation through a transonic fan 52nd Aiaa/Sae/Asee Joint Propulsion Conference, 2016. |
0.44 |
|
| 2016 |
Spencer RA, Gorrell SE, Jones MR, Duque EPN. Analysis and comparison of inlet distortion flow physics at design and near stall operating condition using proper orthogonal decomposition 52nd Aiaa/Sae/Asee Joint Propulsion Conference, 2016. |
0.407 |
|
| 2015 |
Weston DB, Gorrell SE, Marshall ML, Wallis CV. Analysis of turbofan performance under total pressure distortion at various operating points Proceedings of the Asme Turbo Expo. 2. DOI: 10.1115/GT2015-42879 |
0.419 |
|
| 2015 |
Clark KP, Gorrell SE. Analysis and prediction of shock-induced vortex circulation in transonic compressors Journal of Turbomachinery. 137. DOI: 10.1115/1.4031424 |
0.388 |
|
| 2013 |
Cluff RC, Lundgreen RK, Gorrell SE, Maynes D, Oliphant K. A comparison of three-bladed and four-bladed inducers at on and off design flow rates 49th Aiaa/Asme/Sae/Asee Joint Propulsion Conference. |
0.42 |
|
| 2013 |
Marshall ML, Weston DB, Gorrell SE, Wallis CV. Validation of OVERFLOW 2.2 for use with turbomachinery 49th Aiaa/Asme/Sae/Asee Joint Propulsion Conference. |
0.378 |
|
| 2013 |
Blanc TJ, Gorrell SE, Jones MR, Duque EPN. Analysis and compression of time-accurate turbomachinery simulations using proper orthogonal decomposition 49th Aiaa/Asme/Sae/Asee Joint Propulsion Conference. |
0.345 |
|
| 2012 |
Reynolds SB, Gorrell SE, Estevadeordal J. Particle image velocimetry analysis on the effect of stator loading on transonic blade-row interactions Journal of Turbomachinery. 134. DOI: 10.1115/1.4006585 |
0.617 |
|
| 2011 |
Turner MG, Gorrell SE, Car D. Radial migration of shed vortices in a transonic rotor following a wake generator: A comparison between time accurate and average passage approaches Journal of Turbomachinery. 133. DOI: 10.1115/1.4001241 |
0.472 |
|
| 2011 |
Nolan SPR, Botros BB, Tan CS, Adamczyk JJ, Greitzer EM, Gorrell SE. Effects of upstream wake phasing on transonic axial compressor performance Journal of Turbomachinery. 133. DOI: 10.1115/1.4000572 |
0.524 |
|
| 2011 |
Gibson JR, Gorrell SE. Direct numerical simulation of transonic wake propagation in the presence of an adverse pressure gradient and streamline curvature 41st Aiaa Fluid Dynamics Conference and Exhibit. |
0.34 |
|
| 2010 |
Cho CH, Cho SY, Gorrell SE, Ahn KY, Kim YC. An inverse design of a double-pitch passage for an infinite cascade model experiment Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science. 224: 157-167. DOI: 10.1243/09544062JMES1552 |
0.431 |
|
| 2010 |
Reynolds SB, Gorrell SE, Estevadeordal J. PIV analysis on the effect of stator loading on transonic blade-row interactions Proceedings of the Asme Turbo Expo. 7: 2419-2430. DOI: 10.1115/GT2010-22576 |
0.561 |
|
| 2010 |
Packard NO, Japikse D, Maynes RD, Gorrell SE. Numerical characterization of the inlet flow for eleven radial turbomachines Proceedings of the Asme Turbo Expo. 7: 1779-1791. DOI: 10.1115/GT2010-22366 |
0.443 |
|
| 2010 |
Yao J, Gorrell SE, Wadia AR. High-fidelity numerical analysis of per-rev-type inlet distortion transfer in multistage fans-Part II: Entire component simulation and investigation Journal of Turbomachinery. 132: 1-17. DOI: 10.1115/1.3148479 |
0.486 |
|
| 2010 |
Yao J, Gorrell SE, Wadia AR. High-fidelity numerical analysis of Per-Rev-Type inlet distortion transfer in multistage fans-Part I: Simulations with selected blade rows Journal of Turbomachinery. 132: 1-10. DOI: 10.1115/1.3148478 |
0.467 |
|
| 2010 |
List MG, Gorrell SE, Turner MG. Investigation of Loss Generation in an Embedded Transonic Fan Stage at Several Gaps Using High-Fidelity, Time-Accurate Computational Fluid Dynamics Journal of Turbomachinery. 132. DOI: 10.1115/1.3072522 |
0.635 |
|
| 2010 |
Yao J, Cargill PL, Holmes DG, Gorrell SE. Aspects of numerical analysis for unsteady flows in aircraft engines 48th Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. |
0.373 |
|
| 2009 |
Gorrell SE, Yao J, List MG. Full annulus high fidelity fan and compressor simulations Department of Defense Proceedings of the High Performance Computing Modernization Program - Users Group Conference, Hpcmp-Ugc 2009. 46-56. DOI: 10.1109/HPCMP-UGC.2009.13 |
0.317 |
|
| 2009 |
Rogers DR, Gorrell SE, Bons JP, Snyder DO. Optimization of wind tunnel walls to simulate periodic boundary conditions 47th Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. |
0.424 |
|
| 2008 |
List MG, Gorrell SE, Turner MG. Investigation of loss generation in an embedded transonic fan stage at several gaps using high fidelity, time-accurate CFD Proceedings of the Asme Turbo Expo. 6: 2599-2609. DOI: 10.1115/GT2008-51220 |
0.576 |
|
| 2008 |
Yao J, Gorrell SE, Wadia AR. High-fidelity numerical analysis of per-rev-type inlet distortion transfer in multistage fans - part II : Entire component simulation and investigation Proceedings of the Asme Turbo Expo. 6: 469-480. DOI: 10.1115/GT2008-50813 |
0.383 |
|
| 2008 |
Yao J, Gorrell SE, Wadia AR. High-fidelity numerical analysis of per-rev-type inlet distortion transfer in multistage fans - part I : Simulations with selected blade rows Proceedings of the Asme Turbo Expo. 6: 457-467. DOI: 10.1115/GT2008-50812 |
0.374 |
|
| 2008 |
Wadia AR, Yao J, Gorrell SE. Numerical investigation of inlet distortion induced swirl in multistage fans Icas Secretariat - 26th Congress of International Council of the Aeronautical Sciences 2008, Icas 2008. 6: 462-471. |
0.351 |
|
| 2008 |
Gorrell SE, Yao J, Wadia AR. High fidelity URANS analysis of swirl generation and fan response to inlet distortion 44th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit. |
0.435 |
|
| 2007 |
Estevadeordal J, Gorrell SE, Copenhaver WW. PIV study of wake-rotor interactions in a transonic compressor at various operating conditions Journal of Propulsion and Power. 23: 235-242. DOI: 10.2514/1.17452 |
0.584 |
|
| 2007 |
Gorrell SE, Van De Wall A, Tsung FL. Understanding unsteady flow features in transonic compressors Computing in Science and Engineering. 9: 12-17. DOI: 10.1109/Mcse.2007.130 |
0.438 |
|
| 2007 |
List MG, Gorrell SE, Turner MG, Nimersheim JA. High fidelity modeling of blade row interaction in a transonic compressor Collection of Technical Papers - 43rd Aiaa/Asme/Sae/Asee Joint Propulsion Conference. 1: 424-437. |
0.508 |
|
| 2007 |
Jixian Y, Gorrell SE, Wadia AR. A time-accurate CFD analysis of inlet distortion induced swirl in multistage fans Collection of Technical Papers - 43rd Aiaa/Asme/Sae/Asee Joint Propulsion Conference. 1: 628-641. |
0.373 |
|
| 2006 |
Gorrell SE, Car D, Puterbaugh SL, Estevadeordal J, Okiishi TH. An investigation of wake-shock interactions in a transonic compressor with digital particle image velocimetry and time-accurate computational fluid dynamics Journal of Turbomachinery. 128: 616-626. DOI: 10.1115/1.2220049 |
0.731 |
|
| 2006 |
Gorrell SE, Yao J, Tsung FL, Vickery R. Computational science and engineering advances understanding of complex unsteady flows in high performance fans and compressors Proceedings - Hpcmp Users Group Conference, Ugc 2006. 31-38. DOI: 10.1109/HPCMP-UGC.2006.15 |
0.355 |
|
| 2006 |
Gorrell SE. Computational science and engineering applied to military fan and compressor design Collection of Technical Papers - 44th Aiaa Aerospace Sciences Meeting. 15: 11349-11357. |
0.337 |
|
| 2006 |
Turner MG, Gorrell SE, Car D. A model of compressor blade row interaction with shock induced vortex shedding Collection of Technical Papers - Aiaa/Asme/Sae/Asee 42nd Joint Propulsion Conference. 2: 1410-1422. |
0.398 |
|
| 2005 |
Gorrell SE, Car D, Puterbaugh SL, Estevadeordal J, Okiishi TH. An investigation of wake-shock interactions in a transonic compressor with DPIV and time-accurate CFD Proceedings of the Asme Turbo Expo. 6: 1499-1511. DOI: 10.1115/GT2005-69107 |
0.744 |
|
| 2003 |
Gorrell SE, Okiishi TH, Copenhaver WW. Stator-rotor interactions in a transonic compressor - Part 2: Description of a loss-producing mechanism Journal of Turbomachinery. 125: 336-345. DOI: 10.1115/1.1540120 |
0.726 |
|
| 2003 |
Gorrell SE, Okiishi TH, Copenhaver WW. Stator-rotor interactions in a transonic compressor - Part 1: Effect of blade-row spacing on performance Journal of Turbomachinery. 125: 328-335. DOI: 10.1115/1.1540119 |
0.736 |
|
| 2002 |
Gorrell SE, Okiishi TH, Copenhaver WW. Stator-rotor interactions in a transonic compressor: Part 2 - Description of a loss producing mechanism American Society of Mechanical Engineers, International Gas Turbine Institute, Turbo Expo (Publication) Igti. 5: 899-911. DOI: 10.1115/GT2002-30495 |
0.727 |
|
| 2002 |
Gorrell SE, Okiishi TH. Stator-rotor interactions in a transonic compressor: Part 1 - Effect of blade-row spacing on performance American Society of Mechanical Engineers, International Gas Turbine Institute, Turbo Expo (Publication) Igti. 5: 889-898. DOI: 10.1115/GT2002-30494 |
0.739 |
|
| 2002 |
Estevadeordal J, Gogineni S, Goss L, Copenhaver W, Gorrell S. Study of wake-blade interactions in a transonic compressor using flow visualization and DPIV Journal of Fluids Engineering, Transactions of the Asme. 124: 166-175. DOI: 10.1115/1.1429638 |
0.53 |
|
| 2002 |
Copenhaver W, Estevadeordal J, Gogineni S, Gorrell S, Goss L. DPIV study of near-stall wake-rotor interactions in a transonic compressor Experiments in Fluids. 33: 899-908. DOI: 10.1007/S00348-002-0503-Y |
0.531 |
|
| 2001 |
Gorrell SE, Copenhaver WW, Chriss RM. Upstream wake influences on the measured performance of a transonic compressor stage Journal of Propulsion and Power. 17: 43-48. DOI: 10.2514/2.5705 |
0.513 |
|
| 2001 |
Estevadeordal J, Gogineni S, Goss L, Copenhaver W, Gorrell S. 4. Vortex-shedding in a transonic compressor Journal of Visualization. 3: 310-310. DOI: 10.1007/Bf03181722 |
0.457 |
|
| 2000 |
Estevadeordal J, Gogineni S, Goss L, Copenhaver W, Gorrell S. 1. Visualization of Vortex-Shedding and blade synchronization in a transonic compressor Journal of Visualization. 3: 95-95. DOI: 10.1007/Bf03182397 |
0.312 |
|
| 1999 |
Chriss RM, Copenhaver WW, Gorrell SE. The effects of blade-row spacing on the flow capacity of a transonic rotor Proceedings of the Asme Turbo Expo. 1. DOI: 10.1115/99-GT-209 |
0.562 |
|
| 1994 |
Gorrell SE, Russler PM. Stall inception in a high -speed low aspect ratio fan including the effects of casing treatments Proceedings of the Asme Turbo Expo. 1. DOI: 10.1115/94-GT-322 |
0.375 |
|
| 1994 |
Gorrell SE, Russler PM. Stall inception in a high-speed low aspect ratio fan including the effects of casing treatments American Society of Mechanical Engineers (Paper). 1-12. |
0.372 |
|
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