Joaquim Martins

Last updated
Martins, Joaquim R. R. A.; Ning, Andrew (2022). Engineering Design Optimization. Cambridge: Cambridge University Press. ISBN   978-1108833417.

Selected articles

  • Martins, J. R. R. A., Sturdza, P., and Alonso, J. J. (2003). The complex-step derivative approximation. ACM Transactions on Mathematical Software (TOMS), 29(3), 245–262. doi: 10.1145/838250.838251
  • Martins, J. R. R. A., and Lambe, A. B. (2013). Multidisciplinary design optimization: a survey of architectures. AIAA journal, 51(9), 2049–2075. doi: 10.2514/1.J051895
  • Gray, J. S., Hwang, J. T., Martins, J. R. R. A., Moore, K. T., and Naylor, B. A. (2019). OpenMDAO: An open-source framework for multidisciplinary design, analysis, and optimization. Structural and Multidisciplinary Optimization, 59, 1075–1104. doi: 10.1007/s00158-019-02211-z
  • Brelje, B. J., & Martins, J. R. R. A. (2019). Electric, hybrid, and turboelectric fixed-wing aircraft: A review of concepts, models, and design approaches. Progress in Aerospace Sciences, 104, 1–19. doi: 10.1016/j.paerosci.2018.06.004
  • Martins, J. R. (2022). Aerodynamic design optimization: Challenges and perspectives. Computers & Fluids, 239, 105391. doi: 10.1016/j.compfluid.2022.105391
  • Adler, E. J., & Martins, J. R. (2023). Hydrogen-powered aircraft: fundamental concepts, key technologies, and environmental impacts. Progress in Aerospace Sciences, 141, 100922. doi: 10.1016/j.paerosci.2023.100922

Related Research Articles

Multi-disciplinary design optimization (MDO) is a field of engineering that uses optimization methods to solve design problems incorporating a number of disciplines. It is also known as multidisciplinary system design optimization (MSDO), and multidisciplinary design analysis and optimization (MDAO).

<span class="mw-page-title-main">Wing root</span> Portion of aircraft wing

The wing root is the part of the wing on a fixed-wing aircraft or winged-spaceship that is closest to the fuselage, and is the junction of the wing with the fuselage. The term is also used for the junction of the wing with the opposite wing, ie on the fuselage centerline, as with the upper wing of a biplane. The opposite end of a wing from the wing root is the wing tip.

Daniel P. Raymer is an aerospace design engineer widely recognized as an expert in the fields of aircraft conceptual design, design engineering, aircraft configuration, and layout.

Wing-shape optimization is a software implementation of shape optimization primarily used for aircraft design. This allows for engineers to produce more efficient and cheaper aircraft designs.

modeFRONTIER is a software solution for simulation process automation and design exploration developed by ESTECO, an Italian engineering software house. modeFRONTIER leverages advanced optimization algorithms and methodologies and enables engineers to find optimal solutions for complex engineering problems. Its workflow-based environment and multi-objective optimization algorithms are used for streamlining the engineering design process and obtaining improved results.

Value-driven design (VDD) is a systems engineering strategy based on microeconomics which enables multidisciplinary design optimization. Value-driven design is being developed by the American Institute of Aeronautics and Astronautics, through a program committee of government, industry and academic representatives. In parallel, the U.S. Defense Advanced Research Projects Agency has promulgated an identical strategy, calling it value-centric design, on the F6 Program. At this point, the terms value-driven design and value-centric design are interchangeable. The essence of these strategies is that design choices are made to maximize system value rather than to meet performance requirements.

John H. McMasters was an aeronautical engineer notable for his contributions to aerodynamics and engineering education.

ModelCenter, developed by Phoenix Integration, is a software package that aids in the design and optimization of systems. It enables users to conduct trade studies, as well as optimize designs. It interfaces with other common modeling tools, including Systems Tool Kit, PTC Integrity Modeler, IBM Rhapsody, No Magic, Matlab, Nastran, Microsoft Excel, and Wolfram SystemModeler. ModelCenter also has tools to enable collaboration among design team members.

OpenMDAO is an open-source high-performance computing platform for systems analysis and multidisciplinary optimization written in the Python programming language.

The service-oriented computing environment (SORCER) is a distributed computing platform implemented in Java. It allows writing network-programs that operate on wrapped applications (services) to spread across the network. SORCER is often utilized in scenarios similar to those where grids are used in order to run parallel tasks.

<span class="mw-page-title-main">Olivier de Weck</span> Professor of Astronautics and Systems Engineering

Olivier L. de Weck is the Apollo Program Professor of Astronautics and Engineering Systems at the Massachusetts Institute of Technology (MIT). He has authored and co-authored more than 400 peer-reviewed publications. He is a Fellow of the INCOSE and a Fellow of the AIAA. He is the Editor-in-Chief of the Journal of Spacecraft and Rockets. From 2013-2018 de Weck served as the Editor-in-Chief for Systems Engineering, the leading journal of INCOSE. He is best known for contributions to the fields of Systems Engineering, Design optimization, and Space Logistics, where together with colleagues from JPL he coined the term Interplanetary Supply Chain. More recently he has become active in the field of Remote Sensing.

Gradient-enhanced kriging (GEK) is a surrogate modeling technique used in engineering. A surrogate model is a prediction of the output of an expensive computer code. This prediction is based on a small number of evaluations of the expensive computer code.

Robert E. "Rob" Meyerson is an American aerospace engineer and executive.

<span class="mw-page-title-main">Blade-vortex interaction</span>

A blade vortex interaction (BVI) is an unsteady phenomenon of three-dimensional nature, which occurs when a rotor blade passes within a close proximity of the shed tip vortices from a previous blade. The aerodynamic interactions represent an important topic of investigation in rotorcraft research field due to the adverse influence produced on rotor noise, particularly in low speed descending flight condition or maneuver, which generates high amplitude impulsive noise.

Guru Guruswamy is an American engineer working as Principal Scientist at Ames Research Center since 1988. He pioneered research in the area of computational aeroelasticity that involves Unsteady Aerodynamics, Finite Element Methods, Computational Fluid Dynamics, Parallel Computing and Problem Solving Environment. His innovative research was utilized in the first commercial 3-D computational aeroelasticity software developed by a major aerospace industry. The aeroelasticity legend Holt Ashley extensively referred to Guruswamy's research in his classical review paper. In 1988 he demonstrated the unique use of Transonic Small Perturbation based CFD for designing active controls to increase the safety of aircraft. It was followed by a break through development of Euler flow equations based Computational Aeroelasticy. It was cited by another Aeroelasticity legend John Dugundji of MIT as an important milestone in Aeroelasticity. A google search shows about 150 researchers took advantage Guruswamy's work based on the Euler equations for follow-up developments.

Achille Messac is the Dean of the College of Engineering, Architecture and Computer Sciences at Howard University. He has previously served as Professor of Aerospace Engineering Mississippi State University. He was elected a Fellow of the American Association for the Advancement of Science in 2019.

<span class="mw-page-title-main">OpenVSP</span> Open source parametric aircraft geometry tool

OpenVSP, also known as Open Vehicle Sketch Pad, is an open source parametric aircraft geometry tool originally developed by NASA. It can be used to create 3D models of aircraft and to support engineering analysis of those models. Predecessors to OpenVSP including VSP and Rapid Aircraft Modeler (RAM) were developed by J.R. Gloudemans and others for NASA beginning in the early 1990s. OpenVSP v2.0 was released as open source under the NOSA license in January 2012. Development has been led by Rob McDonald since around 2012 and has been supported by NASA and AFRL among other contributions.

<span class="mw-page-title-main">Carlos Cesnik</span> Brazilian-American aerospace engineer

Carlos E. S. Cesnik is a Brazilian-American aerospace engineer, academic, and author. He is the Clarence L. (Kelly) Johnson Collegiate Professor of Aerospace Engineering and the founding Director of the Active Aeroelasticity and Structures Research Laboratory at the University of Michigan. He also directs the Airbus-Michigan Center for Aero-Servo-Elasticity of Very Flexible Aircraft (CASE-VFA).

<span class="mw-page-title-main">Marty Bradley</span> American aerospace engineer

Marty Bradley is an American aerospace engineer who specializes in advanced propulsion, electric aircraft, and sustainable aviation. He is a fellow of the American Institute of Aeronautics and Astronautics (AIAA), an adjunct professor of aerospace and mechanical engineering practice at the University of Southern California (USC), and a sustainable aviation consultant.

<span class="mw-page-title-main">Pauline Sherman</span> American aerospace engineer and academic

Pauline Mont Sherman was an American aerospace engineer and academic. She was the first female Professor in the College of Engineering at the University of Michigan and also the first woman to become Professor of Aerospace Engineering at the University of Michigan. Her research focuses on jet noise, low-density flows, two-phase flows, and especially hypersonic flows.

References

  1. "Joaquim R. R. A. Martins". aero.engin.umich.edu.
  2. "Home · MDO Lab". mdolab.engin.umich.edu.
  3. 1 2 "Joaquim Martins R. R. A." name.engin.umich.edu.
  4. McAlpine, Kate (April 5, 2021). "Streamlining aircraft". Michigan Engineering News.
  5. "Engineering Design Optimization". mdobook.github.io.
  6. "Joaquim R. R. A. Martins". www.
  7. 1 2 "William F. Ballhaus Prize | Aeronautics and Astronautics". aa.stanford.edu.
  8. "People · Joaquim R. R. A. Martins". mdolab.engin.umich.edu.
  9. "Martins named Pauline M. Sherman Collegiate Professor of Aerospace Engineering". aero.engin.umich.edu. April 12, 2022.
  10. "Multidisciplinary Design Optimization for Complex Engineered Systems Design: Report from an NSF Workshop · MDO Lab". mdolab.engin.umich.edu.
  11. "UTIAS-MITACS International Workshop on Aviation and Climate Change". goldfinger.utias.utoronto.ca.
  12. Lambe, Andrew B.; Martins, Joaquim R. R. A. (August 2012). "Extensions to the design structure matrix for the description of multidisciplinary design, analysis, and optimization processes". Structural and Multidisciplinary Optimization. 46 (2): 273–284. doi:10.1007/s00158-012-0763-y. S2CID   253688924.
  13. Martins, Joaquim R. R. A.; Lambe, Andrew B. (September 2013). "Multidisciplinary Design Optimization: A Survey of Architectures". AIAA Journal. 51 (9): 2049–2075. Bibcode:2013AIAAJ..51.2049M. doi:10.2514/1.J051895.
  14. Martins, Joaquim R.R.A. (May 2022). "Aerodynamic design optimization: Challenges and perspectives". Computers & Fluids. 239: 105391. doi: 10.1016/j.compfluid.2022.105391 .
  15. He, Ping; Mader, Charles A.; Martins, Joaquim R.R.A.; Maki, Kevin J. (May 2018). "An aerodynamic design optimization framework using a discrete adjoint approach with OpenFOAM". Computers & Fluids. 168: 285–303. doi:10.1016/j.compfluid.2018.04.012.
  16. Madsen, Mads H. Aa.; Zahle, Frederik; Sørensen, Niels N.; Martins, Joaquim R. R. A. (3 April 2019). "Multipoint high-fidelity CFD-based aerodynamic shape optimization of a 10 MW wind turbine". Wind Energy Science. 4 (2): 163–192. Bibcode:2019WiEnS...4..163M. doi: 10.5194/wes-4-163-2019 .
  17. Garg, Nitin; Pearce, Bryce W.; Brandner, Paul A.; Phillips, Andrew W.; Martins, Joaquim R.R.A.; Young, Yin L. (January 2019). "Experimental investigation of a hydrofoil designed via hydrostructural optimization". Journal of Fluids and Structures. 84: 243–262. Bibcode:2019JFS....84..243G. doi: 10.1016/j.jfluidstructs.2018.10.010 .
  18. Lyu, Zhoujie; Kenway, Gaetan K. W.; Martins, Joaquim R. R. A. (April 2015). "Aerodynamic Shape Optimization Investigations of the Common Research Model Wing Benchmark". AIAA Journal. 53 (4): 968–985. Bibcode:2015AIAAJ..53..968L. doi:10.2514/1.J053318. hdl: 2027.42/140684 .
  19. Kenway, Gaetan K. W.; Kennedy, Graeme J.; Martins, Joaquim R. R. A. (May 2014). "Scalable Parallel Approach for High-Fidelity Steady-State Aeroelastic Analysis and Adjoint Derivative Computations". AIAA Journal. 52 (5): 935–951. Bibcode:2014AIAAJ..52..935K. doi:10.2514/1.J052255. hdl: 2027.42/140671 . S2CID   1414020.
  20. 1 2 Kenway, Gaetan K. W.; Martins, Joaquim R. R. A. (January 2014). "Multipoint High-Fidelity Aerostructural Optimization of a Transport Aircraft Configuration". Journal of Aircraft. 51 (1): 144–160. doi:10.2514/1.C032150. hdl: 2027.42/140504 .
  21. Yildirim, Anil; Gray, Justin S.; Mader, Charles A.; Martins, Joaquim R. R. A. (July 2022). "Boundary-Layer Ingestion Benefit for the STARC-ABL Concept". Journal of Aircraft. 59 (4): 896–911. doi:10.2514/1.C036103. S2CID   246785594.
  22. Anibal, Joshua L.; Mader, Charles A.; Martins, Joaquim R.R.A. (June 2022). "Aerodynamic shape optimization of an electric aircraft motor surface heat exchanger with conjugate heat transfer constraint". International Journal of Heat and Mass Transfer. 189: 122689. doi: 10.1016/j.ijheatmasstransfer.2022.122689 .
  23. Martins, Joaquim R.R.A.; Alonso, Juan J.; Reuther, James J. (March 2005). "A Coupled-Adjoint Sensitivity Analysis Method for High-Fidelity Aero-Structural Design". Optimization and Engineering. 6 (1): 33–62. doi:10.1023/B:OPTE.0000048536.47956.62. S2CID   2726824.
  24. Brooks, Timothy R.; Kenway, Gaetan K. W.; Martins, Joaquim R. R. A. (July 2018). "Benchmark Aerostructural Models for the Study of Transonic Aircraft Wings". AIAA Journal. 56 (7): 2840–2855. Bibcode:2018AIAAJ..56.2840B. doi: 10.2514/1.J056603 .
  25. Bons, Nicolas P.; Martins, Joaquim R. R. A.; Odaguil, Felipe I. K.; Cuco, Ana Paula C. (2022). "Aerostructural Wing Optimization of a Regional Jet Considering Mission Fuel Burn". ASME Open Journal of Engineering. 1. doi: 10.1115/1.4055630 .
  26. Mangano, Marco; He, Sicheng; Liao, Yingqian; Caprace, Denis-Gabriel; Martins, Joaquim R. (2022). "Towards Passive Aeroelastic Tailoring of Large Wind Turbines Using High-Fidelity Multidisciplinary Design Optimization". AIAA SCITECH 2022 Forum. doi:10.2514/6.2022-1289. ISBN   978-1-62410-631-6.
  27. Garg, Nitin; Kenway, Gaetan K.W.; Martins, Joaquim R.R.A.; Young, Yin Lu (May 2017). "High-fidelity multipoint hydrostructural optimization of a 3-D hydrofoil". Journal of Fluids and Structures. 71: 15–39. Bibcode:2017JFS....71...15G. doi:10.1016/j.jfluidstructs.2017.02.001.
  28. Hwang, John T.; Martins, Joaquim R.R.A. (31 December 2018). "A Computational Architecture for Coupling Heterogeneous Numerical Models and Computing Coupled Derivatives". ACM Transactions on Mathematical Software. 44 (4): 1–39. doi: 10.1145/3182393 .
  29. Gray, Justin S.; Hwang, John T.; Martins, Joaquim R. R. A.; Moore, Kenneth T.; Naylor, Bret A. (April 2019). "OpenMDAO: an open-source framework for multidisciplinary design, analysis, and optimization". Structural and Multidisciplinary Optimization. 59 (4): 1075–1104. doi: 10.1007/s00158-019-02211-z .
  30. "Engineering Design Optimization Joaquim R. R. A. Martins, Andrew Ning" (PDF).
  31. Wu, Neil; Kenway, Gaetan; Mader, Charles; Jasa, John; Martins, Joaquim (24 October 2020). "pyOptSparse: A Python framework for large-scale constrained nonlinear optimization of sparse systems". Journal of Open Source Software. 5 (54): 2564. Bibcode:2020JOSS....5.2564W. doi: 10.21105/joss.02564 .
  32. Bouhlel, Mohamed Amine; He, Sicheng; Martins, Joaquim R. R. A. (April 2020). "Scalable gradient–enhanced artificial neural networks for airfoil shape design in the subsonic and transonic regimes". Structural and Multidisciplinary Optimization. 61 (4): 1363–1376. doi:10.1007/s00158-020-02488-5. S2CID   253683318.
  33. Bouhlel, Mohamed Amine; Hwang, John T.; Bartoli, Nathalie; Lafage, Rémi; Morlier, Joseph; Martins, Joaquim R.R.A. (2019). "A Python surrogate modeling framework with derivatives". Advances in Engineering Software. 135. doi:10.1016/j.advengsoft.2019.03.005.
  34. 12th AIAA Aviation Technology, Integration, and Operations (ATIO) Conference and 14th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference. 2012. doi:10.2514/MATIO12. ISBN   978-1-60086-930-3.
  35. "Congratulations to Prof. Joaquim Martins and Marco Mangano on 2019 AIAA Applied Aerodynamics Best Paper Award". aero.engin.umich.edu. April 19, 2019.
  36. "Engineering Design Optimization" (PDF).
Joaquim R. R. A. Martins
Joaquim Martins.jpg
Born
Nationality Portugal, Norway, United States
Occupation(s) Aerospace engineer, academic and author
Academic background
EducationM.Eng. Aeronautics
M.Sc. Aeronautics and Astronautics
Ph.D. Aeronautics and Astronautics
Alma mater Stanford University
Imperial College London
Thesis A coupled-adjoint method for high-fidelity aero-structural optimization  (2002)