Referencing pyNastran (AIAA Format)

Official Release

Doyle, S., “PyNastran: A Python-based interface tool for Nastran’s file formats”, Version 1.3.4, https://github.com/SteveDoyle2/pyNastran.

Dev Release

Doyle, S., “PyNastran: A Python-based interface tool for Nastran’s file formats”, Version 1.4.0+dev.ed62bb134, https://github.com/SteveDoyle2/pyNastran.

You can access the version by typing the following on the command line:
  • pyNastranGUI –version

If you get a no checksum error (you didn’t checkout the code from git), use:

Doyle, S., “PyNastran: A Python-based interface tool for Nastran’s file formats”, Accessed 19 January 2024, https://github.com/SteveDoyle2/pyNastran.

References to pyNastran

Commercial/Government

  1. S. Doyle, J. Robinson, V. Ho, G. Ogawa and M. Baker, "Aeroelastic Optimization of Wing Structure Using Curvilinear Spars and Ribs (SpaRibs) and SpaRibMorph," in AIAA, 2017.
  2. J. Robinson, S. Doyle, G. Ogawa, M. Baker, S. De, M. Jrad, R. Kapania and C.-G. Pak, "Aeroelastic Optimization of Wing Structure Using Curvilinear Spars and Ribs (SpaRibs)," in 58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, AIAA SciTech Forum, 2016.
  3. Reasor, D. A., Bhamidipati, K. K., and Chin A. W. "X-56A Aeroelastic Flight Test Predictions,". Edwards Air Force Base, CA. 54th AIAA Aerospace Sciences Meeeting. San Diego, CA. AIAA 2016-1053. 2016.
  4. R. Palacios and A. Cea, "Nonlinear Modal Condensation of Large Finite Element Models: Application of Hodges’s Intrinsic Theory," AIAA Journal: Special Section on Asymptotic Analyses, Dynamics, and Aeroelasticity, vol. 57, no. 10, pp. 4255-4268, October 2019.
  5. P. Beran, E. Forester, Schrock and Chris, "Adaptive Multi-Fidelity Methods for Physics-Based Decision-Making," AFOSR Computational Mathematics Program Review, Arlington, VA, 2017.
  6. H. v. Weers and S. Vyas, "Thermal Simulation with OpenModelica of the X-IFU Focal Plane in the Athena X-ray Space Observatory," Netherlands Institute for Space Research, 2019.

Academia

  1. B. M. Nickerson, "Development of an Integrated Numerical Method for the Fatigue Analysis of Railway Bogies," Faculty of Engineering at Stellenbosch University: Master of Engineering (Mechanical), Western Cape, South Africa, 2017.
  2. M. Ghienne, "Doctoral Thesis: Design and Characterization of Bolted Connections for Robust Reduction of structural Vibrations," Conservatoire national des arts et métiers (CNAM), Paris, France, 2017.
  3. B. M. Sauerer, "• Order-reduced simulation models and consideration of additive manufacturing in the mathematical optimization of mechanical structures," Technical University of Munich, Munich, Germany, 2017.
  4. V. S. d. Santos and H. Pegado, "Use of Third-Order Piston Theory in Panel Flutter Analysis on Composite Laminated Plaets with NASTRAN," Xli Cilamce, Foz do Iguaçu, Brazil, 2020.
  5. J. H. Bussemaker, "Wing Optimization with Active Load Control," Delft University of Technology, Holland, Netherlands, 2018.
  6. L. B. Soriano, "Validation and Extension of an MDO Frameword including Dynamic Aeroelastic Analysis," University of Madrid, Madrid, CA, 2020.

Software

  1. J. S. Gray, J. T. Hwang, J. R. R. A. Martins, K. T. Moore and B. A. Naylor, "OpenMDAO: An Open-Source Framework for Multidisciplinary Design, Analysis, and Optimization," in Structural and Multidisciplinary Optimization, 2019.
  2. J. Deaton, "Multidisciplinary-design Adaptation and Sensitivity Toolkit (MAST)," Air Force Research Laboratory (AFRL), 24 Jul 2020. [Online]. Available: https://www.mast-multiphysics.com/structural_example_7.html. [Accessed 19 December 2020].
  3. "pSeven Changelog," DataAdvance, [Online]. Available: https://www.datadvance.net/product/pseven/manual/6.17/changelog.html. [Accessed 20 December 2020].