| Reliability-based structural design SK Choi, RV Grandhi, RA Canfield Reliability-based Structural Design, by S.-K. Choi, RV Grandhi, and RA …, 2006 | 1002* | 2006 |
| Polynomial chaos expansion with latin hypercube sampling for estimating response variability SK Choi, RV GRANDHI, RA CANFIELD, CL PETTIT AIAA journal 42 (6), 1191-1198, 2004 | 267 | 2004 |
| An approximation approach for uncertainty quantification using evidence theory HR Bae, RV Grandhi, RA Canfield Reliability Engineering & System Safety 86 (3), 215-225, 2004 | 259 | 2004 |
| Epistemic uncertainty quantification techniques including evidence theory for large-scale structures HR Bae, RV Grandhi, RA Canfield Computers & Structures 82 (13-14), 1101-1112, 2004 | 246 | 2004 |
| ASTROS--A Multidisciplinary Automated Structural Design Tool DJ Neill, EH Johnson, R Canfield Journal of Aircraft 27 (12), 1021-1027, 1990 | 134 | 1990 |
| ASTROS—A multidisciplinary automated structural design tool DJ Neill, EH Johnson, R Canfield Structures, Structural Dynamics and Materials Conference, 28th, Monterey, CA …, 1987 | 134 | 1987 |
| Comparison of evidence theory and Bayesian theory for uncertainty modeling P Soundappan, E Nikolaidis, RT Haftka, R Grandhi, R Canfield Reliability engineering & System safety 85 (1-3), 295-311, 2004 | 133 | 2004 |
| High-quality approximation of eigenvalues in structural optimization RA Canfield AIAA journal 28 (6), 1116-1122, 1990 | 115* | 1990 |
| Uncertainty quantification of structural response using evidence theory HR Bae, RV Grandhi, RA Canfield AIAA journal 41 (10), 2062-2068, 2003 | 109 | 2003 |
| Structural reliability under non-Gaussian stochastic behavior SK Choi, RV Grandhi, RA Canfield Computers & structures 82 (13-14), 1113-1121, 2004 | 105 | 2004 |
| Joined-wing aeroelastic design with geometric nonlinearity M Blair, RA Canfield, RW Roberts Jr Journal of Aircraft 42 (4), 832-848, 2005 | 104 | 2005 |
| A Robust and Reliability-Based Design Optimization Framework for Wing Design R Paiva, A Carvalho, C Crawford, A Suleman, R Canfield 51st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials …, 2010 | 77* | 2010 |
| A joined-wing structural weight modeling study MB Blair, R Canfield 43rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials …, 2002 | 77 | 2002 |
| Sensitivity analysis of structural response uncertainty propagation using evidence theory HR Bae, RV Grandhi, RA Canfield Structural and Multidisciplinary Optimization 31, 270-279, 2006 | 72 | 2006 |
| Multibody dynamic aeroelastic simulation of a folding wing aircraft J Scarlett, R Canfield, B Sanders 47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials …, 2006 | 56 | 2006 |
| Joined-wing sensor-craft configuration design CC Rasmussen, RA Canfield, M Blair Journal of aircraft 43 (5), 1470-1478, 2006 | 54 | 2006 |
| Integrated Structural Design and Vibration Suppression Using Independent Modal Space Control RA Canfield, L Meirovitch AIAA Journal 32 (10), 2053-2060, 1994 | 53 | 1994 |
| Aeroelastic scaling of a joined wing for nonlinear geometric stiffness VL Bond, RA Canfield, A Suleman, M Blair AIAA journal 50 (3), 513-522, 2012 | 49 | 2012 |
| Optimization process for configuration of flexible joined-wing CC Rasmussen, RA Canfield, M Blair Structural and Multidisciplinary Optimization 37, 265-277, 2009 | 47 | 2009 |
| Nonlinear response structural optimization of a joined wing using equivalent loads YI Kim, GJ Park, RM Kolonay, M Blair, RA Canfield AIAA journal 46 (11), 2703-2713, 2008 | 46 | 2008 |
Seung-Kyum ChoiAssociate Professor of Mechanical Engineering, Georgia Institute of TechnologyVahvistettu sähköpostiosoite verkkotunnuksessa me.gatech.edu