| Leading edge modification effects on turbine cascade endwall loss S Becz, MS Majewski, LS Langston Turbo Expo: Power for Land, Sea, and Air 36894, 359-367, 2003 | 89 | 2003 |
| An experimental investigation of contoured leading edges for secondary flow loss reduction S Becz, MS Majewski, LS Langston Turbo Expo: Power for Land, Sea, and Air 41707, 1407-1415, 2004 | 69 | 2004 |
| Design system for managing complexity in aerospace systems S Becz, A Pinto, L Zeidner, R Khire, H Reeve, A Banaszuk 10th AIAA Aviation Technology, Integration, and Operations (ATIO) Conference …, 2010 | 48 | 2010 |
| Measurement and calculation of turbine cascade endwall pressure and shear stress BM Holley, S Becz, LS Langston | 39 | 2006 |
| Measurement and calculation of turbine cascade endwall pressure and shear stress BM Holley, S Becz, LS Langston | 39 | 2006 |
| Attenuation of gas turbine combustor pressure oscillations using symmetry breaking J Cohen, G Hagen, A Banaszuk, S Becz, P Mehta 49th AIAA aerospace sciences meeting including the new horizons forum and …, 2011 | 33 | 2011 |
| Attenuation of gas turbine combustor pressure oscillations using symmetry breaking J Cohen, G Hagen, A Banaszuk, S Becz, P Mehta 49th AIAA aerospace sciences meeting including the new horizons forum and …, 2011 | 33 | 2011 |
| Correct-by-construction design of aircraft electric power systems A Pinto, S Becz, H Reeve 10th AIAA Aviation Technology, Integration, and Operations (ATIO) Conference …, 2010 | 22 | 2010 |
| Architectural enumeration and evaluation for identification of low-complexity systems L Zeidner, H Reeve, R Khire, S Becz 10th AIAA Aviation Technology, Integration, and Operations (ATIO) Conference …, 2010 | 16 | 2010 |
| Analysis of barely visible impact damage for aerospace structures S Becz, J Hurtado, I Lapczyk ICCM-16: 16th Int. Conf. on Composite Materials, 8-13, 2007 | 14 | 2007 |
| Assessing performance uncertainty in complex hybrid systems R Khire, S Becz, H Reeve, L Zeidner 10th AIAA Aviation Technology, Integration, and Operations (ATIO) Conference …, 2010 | 12 | 2010 |
| Design issues for a bottom-up complexity metric applied to hierarchical systems L Zeidner, H Reeve, R Khire, S Becz 10th AIAA Aviation Technology, Integration, and Operations (ATIO) Conference …, 2010 | 6 | 2010 |
| Measurement and calculation of turbine cascade endwall pressure and shear stress BM Holley, S Becz, LS Langston Turbo Expo: Power for Land, Sea, and Air 47306, 497-507, 2005 | 5 | 2005 |
| Gas turbine engine combustor control using emission tomography J Edwards, F Gouldin, S Becz 44th AIAA Aerospace Sciences Meeting and Exhibit, 749, 2006 | 3 | 2006 |
| Characterization of Mixing for a Jet in Crossflow Using Proper Orthogonal Decomposition S Becz, J Cohen 43rd AIAA Aerospace Sciences Meeting and Exhibit, 307, 2005 | 3 | 2005 |
| System complexity reduction via spectral graph partitioning to identify hierarchical modular clusters L Zeidner, A Banaszuk, S Becz 10th AIAA Aviation Technology, Integration, and Operations (ATIO) Conference …, 2010 | 2 | 2010 |
| Leading Edge Modification Effects on Turbine Cascade Endwall S Becz, MS Majewski, LS Langston Paper, ASME, GT-2003-38898, 2003 | 2 | 2003 |
| Dynamic Network Analysis for Robust Uncertainty Management A Banaszuk, JM Pasini, S Becz, ... | | 2010 |
| Emission Tomography for Gas Turbine Combustor Control JL Edwards, FC Gouldin, S Becz PROPER ORTHOGONAL DECOMPOSITION AND TOMOGRAPHIC ANALYSIS OF COMBUSTION …, 2007 | | 2007 |
