Evolving an Aircraft Using a Parametric Design System - Versionsgeschichte

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2015-11-01T11:08:48Z

‎Bibtex

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Gbachelier am 11. Oktober 2014 um 18:37 Uhr

2014-10-11T18:37:13Z

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2014-10-11T08:30:22Z

‎Referenz

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2014-10-10T15:55:18Z

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== Referenz ==
[[Jonathan Byrne]], [[Philip Cardiff]], [[Anthony Brabazon]], [[Michael O’Neill]]: Evolving an Aircraft Using a Parametric Design System. In: [[Literatur_zur_Evolution%C3%A4ren_Kunst#EvoMUSART_2014 | EvoMUSART 2014]], S. 119-130.

== DOI ==
http://link.springer.com/10.1007/978-3-662-44335-4_11

== Abstract ==
Traditional CAD tools generate a static solution to a design problem. Parametric systems allow the user to explore many variations on that design theme. Such systems make the computer a generative design tool and are already used extensively as a rapid prototyping technique in architecture and aeronautics. Combining a design generation tool with an evolutionary algorithm provides a methodology for optimising designs. This works uses NASA’s parametric aircraft design tool (OpenVSP) and an evolutionary algorithm to evolve a range of aircraft that maximise lift and reduce drag while remaining within the framework of the original design. Our approach allows the designer to automatically optimise their chosen design and to generate models with improved aerodynamic efficiency.

== Extended Abstract ==

== Bibtex ==

== Links ==
=== Full Text ===
[extern file]

[[intern file]]

=== Sonstige Links ===
[http://jonathan-byrne.com/presentations/aircraft14.html Jonathan Byrne: Evolving an Aircraft Using a Parametric Design System. Presentation]

@@ Zeile 23: / Zeile 23: @@
   doi={10.1007/978-3-662-44335-4_11},
   title={Evolving an Aircraft Using a Parametric Design System},
-  url={http://dx.doi.org/10.1007/978-3-662-44335-4_11 },
+  url={http://dx.doi.org/10.1007/978-3-662-44335-4_11 http://de.evo-art.org/index.php?title=Evolving_an_Aircraft_Using_a_Parametric_Design_System },
   publisher={Springer Berlin Heidelberg},
   author={Byrne, Jonathan and Cardiff, Philip and Brabazon, Anthony and O’Neill, Michael},

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 == Bibtex ==
+ @incollection{
 == Used References ==

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	== Bibtex ==		== Bibtex ==
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		+
		+	== Used References ==
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		+
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		+
		+	Bollinger, K., Grohmann, M., Tessman, O.: Form, force, performance: Multi-parametric structural design. Architectural Design 78(2), 20–25 (2008)
		+
		+	Cardiff, P., Karač, A., Ivanković, A.: A large strain finite volume method for orthotropic bodies with general material orientations. In: Computer Methods in Applied Mechanics and Engineering (2013)
		+
		+	Day, M.: Grasshopper, generative modelling (2010), http://www.grasshopper3d.com/
		+
		+	Deb, K., Pratap, A., Agarwal, S., Meyarivan, T.: A fast and elitist multiobjective genetic algorithm: NSGA-II. IEEE Transactions on Evolutionary Computation 6(2), 182–197 (2002) ISSN 1089-778X
		+
		+	Dulikravich, G.S.: Aerodynamic shape design and optimization-status and trends. Journal of Aircraft 29(6), 1020–1026 (1992)
		+
		+	Gloudemans, J.R., Davis, P.C., Gelhausen, P.A.: A rapid geometry modeler for conceptual aircraft. In: 34th Aerospace Sciences Meeting and Exhibit, Reno, NV, January, pp. 15–18 (1996)
		+
		+	Holzer, D., Hough, R., Burry, M.: Parametric design and structural optimisation for early design exploration. International Journal of Architectural Computing 5(4), 625–643 (2007)
		+
		+	Jacobs, E.N., Ward, K.E., Pinkerton, R.M.: The characteristics of 78 related airfoil sections from tests in the variable-density wind tunnel. Technical report, DTIC Document (1933)
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		+	Andy Ko, Y.-Y.: The multidisciplinary design optimization of a distributed propulsion blended-wing-body aircraft. PhD thesis, Virginia Polytechnic Institute and State University (2003)
		+
		+	Lawson, B.: How designers think: the design process demystified. Elsevier/Architectural (2006), ISBN 9780750660778, http://books.google.ie/books?id=lPvqZJNAdG8C
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		+	Naujoks, B., Willmes, L., Haase, W., Bäck, T., Schütz, M.: Multi-point airfoil optimization using evolution strategies. In: Proc. European Congress on Computational Methods in Applied Sciences and Engineering (ECCOMAS 2000)(CD-Rom and Book of Abstracts), p. 948 (2000)
		+
		+	Obayashi, S.: Multidisciplinary design optimization of aircraft wing planform based on evolutionary algorithms. In: 1998 IEEE International Conference on Systems, Man, and Cybernetics, vol. 4, pp. 3148–3153. IEEE (1998)
		+
		+	Parmee, I.C., Watson, A.H.: Preliminary airframe design using co-evolutionary multiobjective genetic algorithms. In: Proceedings of the Genetic and Evolutionary Computation Conference, vol. 2, pp. 1657–1665 (1999)
		+
		+	Patankar, S.V., Spalding, D.B.: A calculation procedure for heat, mass and momentum transfer in three-dimensional parabolic flows. International Journal of Heat and Mass Transfer 15(10), 1787–1806 (1972), http://www.sciencedirect.com/science/article/pii/0017931072900543 , doi: http://dx.doi.org/10.1016/0017-9310(72)90054-3, ISSN 0017-9310
		+
		+	Quagliarella, D., D’ambrosio, D., Iollo, A.: Airfoil design using navier-stokes equations and hybrid evolutionary optimization techniques. Technical report, DTIC Document (2003)
		+
		+	Rogalsky, T., Derksen, R.W., Kocabiyik, S.: An aerodynamic design technique for optimizing fan blade spacing. In: Proceedings of the 7th Annual Conference of the Computational Fluid Dynamics Society of Canada, pp. 2–29. Citeseer (1999)
		+
		+	Shea, K., Aish, R., Gourtovaia, M.: Towards integrated performance-driven generative design tools. Automation in Construction 14(2), 253–264 (2005) ISSN 0926-5805
		+
		+	Simon, H.A.: The sciences of the artificial. The MIT Press (1996)
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		+	Oasys Software. GSA, structural analysis version 8.5 (2011), http://www.oasys-software.com/gsa-analysis.html
		+
		+	Bentley Sytems. Generative components, v8i (2011), http://www.bentley.com/getgc/
		+
		+	Weller, H.G., Tabor, G., Jasak, H., Fureby, C.: A tensorial approach to computational continuum mechanics using object-oriented techniques. Computers in physics 12, 620 (1998)
		+
		+	Wüthrich, B., Lee, Y.: Simulation and validation of compressible flow in nozzle geometries and validation of OpenFOAM for this application. PhD thesis, ETH, Swiss Federal Institute of Technology Zurich, Institute of Fluid Dynamics (2007)
		+
		+	Zitzler, E., Thiele, L.: Multiobjective evolutionary algorithms: a comparative case study and the strength Pareto approach. IEEE Trans. Evolutionary Computation 3(4), 257–271 (1999)

	== Links ==		== Links ==

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	=== Sonstige Links ===		=== Sonstige Links ===
−	[http://jonathan-byrne.com/presentations/aircraft14.html Jonathan Byrne: Evolving an Aircraft Using a Parametric Design System. Presentation]	+	[http://jonathan-byrne.com/presentations/aircraft14.html Jonathan Byrne: Evolving an Aircraft Using a Parametric Design System. html-Presentation]

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 == Referenz ==
-[[Jonathan Byrne]], [[Philip Cardiff]], [[Anthony Brabazon]], [[Michael O’Neill]]: Evolving an Aircraft Using a Parametric Design System. In: [[Literatur_zur_Evolution%C3%A4ren_Kunst#EvoMUSART_2014 | EvoMUSART 2014]], S. 119-130.
+[[Jonathan Byrne]], [[Philip Cardiff]], [[Anthony Brabazon]], [[Michael O’Neill]]: Evolving an Aircraft Using a Parametric Design System. In: [[Literatur_zur_Evolution%C3%A4ren_Kunst#EvoMUSART_2014_2 | EvoMUSART 2014]], S. 119-130.
 == DOI ==