The case for open source software in aeronautics-Reference-Cited by-同舟云学术

The case for open source software in aeronautics

Published:2012-05-04 Issue:3 Volume:84 Page:133-139
ISSN:0002-2667
Container-title:Aircraft Engineering and Aerospace Technology
language:en
Short-container-title:

Author:

Ziemer Sven,Stenz Gernot

Abstract

PurposeThe purpose of this paper is to promote the opportunities of open source software (OSS) development in aeronautics. Using the development of an open source framework for conceptual aircraft design as an example, this paper discusses how an inter‐organizational collaboration between industry and academia can build an environment for multi‐disciplinary aircraft design projects.Design/methodology/approachThe paper takes the form of a literature study and comparison of software tools.FindingsThe open source model can facilitate the emergence of a large inter‐organizational community in aeronautics for developing a comprehensive software framework.Practical implicationsDeveloping a general OSS framework for conceptual aircraft design has the potential of attracting a large community for inter‐organizational collaboration on software tools for a multi‐disciplinary optimization (MDO) environment.Originality/valueUsing the concepts of open source in aeronautics has the potential to improve the collaboration among industry and academia on developing software tools for an MDO environment.

Publisher

Emerald

Reference26 articles.

1. Adams, B.M., Bohnhoff, W.J., Dalbey, K.R., Eddy, J.P., Eldred, M.S., Gay, D.M., Haskell, K., Hough, P.D. and Swiler, L.P. (2009), DAKOTA, a Multilevel Parallel Object‐oriented Framework for Design Optimization, Parameter Estimation, Uncertainty Quantification, and Sensitivity Analysis: Version 5.0 User's Manual, Sandia Technical Report SAND2010‐2183, Sandia National Laboratories, Albuquerque, NM.

2. Berndt, J.S. (2011), “JSBSim an open source, platform‐independent, flight dynamics model in C++”, available at: http://jsbsim.sourceforge.net/JSBSimReferenceManual.pdf (accessed 28 October 2011)..

3. Dhondt, G. and Wittig, K. (1998), “Calculix: a free software three‐dimensional structural finite element program”, available at: www.calculix.de/ (accessed 26 July 2011)..

4. Drela, M. (1989), “XFOIL – an analysis and design system for low Reynolds number airfoils”, in Mueller, T. (Ed.), Proceedings of the Conference on Low Reynolds Number Aerodynamics, Notre Dame, IN, USA, 5‐7 June.

5. Drela, M. and Youngren, H. (2007), “AVL (Athena Vortex Lattice)”, available at: http://web.mit.edu/drela/Public/web/avl (accessed 16 July 2011)..

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