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Robert A. Canfield
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Reliability-based structural design
SK Choi, RV Grandhi, RA Canfield
Reliability-based Structural Design, by S.-K. Choi, RV Grandhi, and RA …, 2006
933*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
2632004
An approximation approach for uncertainty quantification using evidence theory
HR Bae, RV Grandhi, RA Canfield
Reliability Engineering & System Safety 86 (3), 215-225, 2004
2512004
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
2402004
ASTROS--A Multidisciplinary Automated Structural Design Tool
DJ Neill, EH Johnson, R Canfield
Journal of Aircraft 27 (12), 1021-1027, 1990
1341990
ASTROS—A multidisciplinary automated structural design tool
DJ Neill, EH Johnson, R Canfield
Structures, Structural Dynamics and Materials Conference, 28th, Monterey, CA …, 1987
1341987
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
1292004
High-quality approximation of eigenvalues in structural optimization
RA Canfield
AIAA journal 28 (6), 1116-1122, 1990
112*1990
Structural reliability under non-Gaussian stochastic behavior
SK Choi, RV Grandhi, RA Canfield
Computers & structures 82 (13-14), 1113-1121, 2004
1092004
Uncertainty quantification of structural response using evidence theory
HR Bae, RV Grandhi, RA Canfield
AIAA journal 41 (10), 2062-2068, 2003
1052003
Joined-wing aeroelastic design with geometric nonlinearity
M Blair, RA Canfield, RW Roberts Jr
Journal of Aircraft 42 (4), 832-848, 2005
1042005
A joined-wing structural weight modeling study
MB Blair, R Canfield
43rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials …, 2002
812002
Sensitivity analysis of structural response uncertainty propagation using evidence theory
HR Bae, RV Grandhi, RA Canfield
Structural and Multidisciplinary Optimization 31, 270-279, 2006
772006
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
75*2010
Joined-wing sensor-craft configuration design
CC Rasmussen, RA Canfield, M Blair
Journal of aircraft 43 (5), 1470-1478, 2006
552006
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
522006
Integrated Structural Design and Vibration Suppression Using Independent Modal Space Control
RA Canfield, L Meirovitch
AIAA Journal 32 (10), 2053-2060, 1994
521994
Sensor-craft structural optimization and analytical certification
RW Roberts, RA Canfield, M Blair
44th AIAA/ASME/ASCE/AHS Structures, Structural Dynamics, and Materials …, 2003
512003
Structural optimization of a joined wing using equivalent static loads
HA Lee, YI Kim, GJ Park, RM Kolonay, M Blair, RA Canfield
Journal of aircraft 44 (4), 1302-1308, 2007
502007
Optimization process for configuration of flexible joined-wing
CC Rasmussen, RA Canfield, M Blair
Structural and Multidisciplinary Optimization 37, 265-277, 2009
472009
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