Abstract
In the aerospace industry the methods of structural optimization have been integrated into the process of engineering design in many cases. Especially for complex design problems, their application leads to optimal layouts which fulfill all requirements in the best possible manner. Fundamental suggestions for this use in industrial practice were made by L.A. Schmit [1]. Nowadays, mathematical optimization algorithms and finite element methods set the basis for optimization computations with a high rate of generality and efficiency [2]. The additional inclusion of optimization models leads not only to a very modular architecture but also to the direct consideration of all relevant practical demands [3]. A variety of examples of aircraft and spacecraft structures shows the advantages of this procedure [4].
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References
Schmit, L.A.: Structural Design by Synthesis, Proc. 2nd Conf. Elet. Comp. ASCE, New York, (1960) 105–122
Atrek, E.; Gallagher, R.H.; Ragsdell, K.M.; Zienkiewicz, O.C.: New Directions in Optimum Structural Design. Chichester, New York, Brisbane, Toronto, Singapore: John Wiley 1984
Eschenauer, H.A.: Rechnerische und experimentelle Untersuchungen zur Strukturoptimierung von Bauteilen, DFG-Forschu ngsbericht. Forschungslaboratorium für Angewandte Strukturoptimierung, Universität-GH Siegen, 1985
Kneppe, G.; Krammer, J.; Winkler, F.: Structural Optimization of Large Scale Problems Using MBB-LAGRANGE, 5th World Congress and Exhibition on FEM, Salzburg (Austria), 1987
Kneppe, G.: Hartzheim, W.: Zimmermann, G.: Development and Application of an Optimization Procedure for Space and Aircraft Structures, Proc. GAMM-Seminar, Discretization Methods and Structural Optimization, Siegen (FR Germany ), 1988
Bisplinghoff, R.L.; Ashley, H.: Principles of Aeroelasticity, New York: Dover Publication 1962
Gödel, H.: Hörnlein, H.: Aeroelasticity and Optimization in Fighter Aircraft Design, AGARD-Report No. 740, Special Course on Fundamentals of Fighter Aircraft Design, 1986
Ross, C.: Strukturoptimierung mit Nebenbedingungen aus der Dynamik. Dissertation. Technische Universität München, to appear 1990
Specht, B.; Helwig, G.: OPOS, A General Computer Package for Optimization of Structures, Report MEB 67/88. Dornier System. Friedrichshafen, 1988
Baier. H.: Structural Control and Optimization of Structures with Constraints in Dynamics. Proceedings 5th Int. Modal Analysis Conf. London, (1987) 903–908
Baier, H.: Algorithmen zur Ermittlung und Charakterisierung Pareto-optimaler Lösungen bei Entwurfsaufgaben für Tragwerke. Zeitschrift für Angewandte Mathematik und Mechanik (ZAMM), Band 57 (1977) 318–320
Dyer, J.S.: A Time-Sharing Computer Program for the Solution of the Multicriteria Problem. Management Science 19 (1973) 1379–1383
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Kneppe, G., Baier, H. (1990). Aircraft and Space Technology. In: Eschenauer, H., Koski, J., Osyczka, A. (eds) Multicriteria Design Optimization. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-48697-5_6
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DOI: https://doi.org/10.1007/978-3-642-48697-5_6
Publisher Name: Springer, Berlin, Heidelberg
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