Suivre
Joaquim R. R. A. Martins
Joaquim R. R. A. Martins
Professor of Aerospace Engineering, University of Michigan
Adresse e-mail validée de umich.edu - Page d'accueil
Titre
Citée par
Citée par
Année
Multidisciplinary design optimization: A survey of architectures
J Martins, AB Lambe
AIAA Journal 59 (9), 2049-2075, 2013
11932013
The complex-step derivative approximation
JRRA Martins, P Sturdza, JJ Alonso
ACM Transactions on Mathematical Software (TOMS) 29 (3), 245-262, 2003
8892003
OpenMDAO: An open-source framework for multidisciplinary design, analysis, and optimization
JS Gray, JT Hwang, JRRA Martins, KT Moore, BA Naylor
Structural and Multidisciplinary Optimization 59, 1075-1104, 2019
5762019
Electric, hybrid, and turboelectric fixed-wing aircraft: A review of concepts, models, and design approaches
BJ Brelje, JRRA Martins
Progress in Aerospace Sciences 104, 1-19, 2019
5342019
Extensions to the design structure matrix for the description of multidisciplinary design, analysis, and optimization processes
AB Lambe, JRRA Martins
Structural and Multidisciplinary Optimization 46, 273-284, 2012
4752012
pyOpt: a Python-based object-oriented framework for nonlinear constrained optimization
RE Perez, PW Jansen, JRRA Martins
Structural and Multidisciplinary Optimization 45, 101-118, 2012
4742012
Multipoint high-fidelity aerostructural optimization of a transport aircraft configuration
GKW Kenway, JRRA Martins
Journal of Aircraft 51 (1), 144-160, 2014
3992014
Review and unification of methods for computing derivatives of multidisciplinary computational models
JRRA Martins, JT Hwang
AIAA Journal 51 (11), 2582-2599, 2013
3832013
Engineering design optimization
JRRA Martins, A Ning
Cambridge University Press, 2021
3462021
High-fidelity aerostructural design optimization of a supersonic business jet
JRRA Martins, JJ Alonso, JJ Reuther
Journal of Aircraft 41 (3), 523-530, 2004
3262004
A Python surrogate modeling framework with derivatives
MA Bouhlel, JT Hwang, N Bartoli, R Lafage, J Morlier, JRRA Martins
Advances in Engineering Software 135, 102662, 2019
3202019
Aerodynamic shape optimization investigations of the common research model wing benchmark
Z Lyu, GKW Kenway, JRRA Martins
AIAA journal 53 (4), 968-985, 2015
3142015
A coupled-adjoint sensitivity analysis method for high-fidelity aero-structural design
JRRA Martins, JJ Alonso, JJ Reuther
Optimization and Engineering 6, 33-62, 2005
2962005
Scalable parallel approach for high-fidelity steady-state aeroelastic analysis and adjoint derivative computations
GKW Kenway, GJ Kennedy, JRRA Martins
AIAA journal 52 (5), 935-951, 2014
2902014
An adaptive approach to constraint aggregation using adjoint sensitivity analysis
NMK Poon, JRRA Martins
Structural and Multidisciplinary Optimization 34, 61-73, 2007
277*2007
Aerodynamic design optimization studies of a blended-wing-body aircraft
Z Lyu, JRRA Martins
Journal of Aircraft 51 (5), 1604-1617, 2014
2592014
An automated method for sensitivity analysis using complex variables
JRRA Martins, IM Kroo, JJ Alonso
AIAA paper 689, 2000, 2000
2472000
A CAD-free approach to high-fidelity aerostructural optimization
G Kenway, G Kennedy, JRRA Martins
13th AIAA/ISSMO multidisciplinary analysis optimization conference, 9231, 2010
2402010
Effective adjoint approaches for computational fluid dynamics
GKW Kenway, CA Mader, P He, JRRA Martins
Progress in Aerospace Sciences 110, 100542, 2019
2292019
ADjoint: an approach for the rapid development of discrete adjoint solvers
CA Mader, JRRA Martins, JJ Alonso, EV Der Weide
AIAA journal 46 (4), 863-873, 2008
2272008
Le système ne peut pas réaliser cette opération maintenant. Veuillez réessayer plus tard.
Articles 1–20