Multidisciplinary Design Optimization of a supersonic transport aircraft using a hybrid genetic/gradient-based algorithm-Reference-Cited by-同舟云学术

Multidisciplinary Design Optimization of a supersonic transport aircraft using a hybrid genetic/gradient-based algorithm

Published:1996-08-22 Issue: Volume: Page:
ISSN:
Container-title:6th Symposium on Multidisciplinary Analysis and Optimization
language:
Short-container-title:

Author:

Bos Dolf¹

Affiliation:

1. Delft Univ. of Technology, Netherlands

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1996-4055

Reference15 articles.

1. Bos,A.H.W.;Multidisdplinanf DesignOptimization of aSecond Generation Supersonic Transport Aircraft usingaHybrid Genetic/ Gradient-guided Algorithm; Ph.D.dissertation,ISBN90-5623-041-7,Delft University of Technology, 1996

2. Chang,K.J.;Haftka,R.T.;Giles,J.L.and Kao, P.J.; Sensitivity-Based Scalingfor Approximating Structural Response; published as AIAA 91-0925. clQBBlc daalqn procedure Figure 5 Comparisonbetweenclassicand

3. Consoli, R.D. and Sobieszczanski-SobieskiJ.; Application of Advanced Multidisciplinary Analysis and Optimization Methods toVehicleDesignSynthesis; ICAS 90-2.3.4.

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