Robert A. Canfield
Title
Cited by
Cited by
Year
Reliability-based structural design
SK Choi, RV Grandhi, RA Canfield
Reliability-based Structural Design, by S.-K. Choi, RV Grandhi, and RA …, 2006
7762006
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
2262004
An approximation approach for uncertainty quantification using evidence theory
HR Bae, RV Grandhi, RA Canfield
Reliability Engineering & System Safety 86 (3), 215-225, 2004
2212004
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
2182004
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
1112004
High-quality approximation of eigenvalues in structural optimization
RA Canfield
AIAA journal 28 (6), 1116-1122, 1990
104*1990
Structural reliability under non-Gaussian stochastic behavior
SK Choi, RV Grandhi, RA Canfield
Computers & structures 82 (13-14), 1113-1121, 2004
1012004
Uncertainty quantification of structural response using evidence theory
HR Bae, RV Grandhi, RA Canfield
AIAA journal 41 (10), 2062-2068, 2003
982003
Joined-wing aeroelastic design with geometric nonlinearity
M Blair, RA Canfield, RW Roberts Jr
Journal of Aircraft 42 (4), 832-848, 2005
962005
A joined-wing structural weight modeling study
MB Blair, R Canfield
43rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials …, 2002
692002
Sensitivity analysis of structural response uncertainty propagation using evidence theory
HR Bae, RV Grandhi, RA Canfield
Structural and Multidisciplinary Optimization 31 (4), 270-279, 2006
662006
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
60*2010
Integrated Structural Design and Vibration Suppression Using Independent Modal Space Control
RA Canfield, L Meirovitch
AIAA Journal 32 (10), 2053-2060, 1994
511994
Joined-wing sensor-craft configuration design
CC Rasmussen, RA Canfield, M Blair
Journal of aircraft 43 (5), 1470-1478, 2006
472006
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
432007
Sensor-craft structural optimization and analytical certification
RW Roberts, RA Canfield, M Blair
44th AIAA/ASME/ASCE/AHS Structures, Structural Dynamics, and Materials …, 2003
432003
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
412006
Optimum design of structures with multiple constraints
RA Canfield, RV Grandhi, VB Venkayya
AIAA journal 26 (1), 78-85, 1988
401988
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