Design of an Aircraft Brake Component Using an Interactive Multidisciplinary Design Optimization Framework
Author:
Stelmack Marc A., Batill Stephen M.1, Beck Bryan C.2
Affiliation:
1. Department of Aerospace and Mechanical Engineering, University of Notre Dame, Notre Dame, IN 46566 2. AlliedSignal Aerospace Aircraft Landing Systems, South Bend, IN 46628
Abstract
A multidisciplinary design optimization (MDO) framework has been used to design an aircraft brake assembly. This was done using a user-interactive implementation of the framework in which design information was obtained from analysis software used in industry but not developed for an MDO application. The design included a number of performance requirements associated with a brake that has been produced for a commercial aircraft. Design improvement was achieved using a practical number of system realizations and the interaction between the optimization algorithm and the design engineers was maintained throughout the process. [S1050-0472(00)00201-4]
Publisher
ASME International
Subject
Computer Graphics and Computer-Aided Design,Computer Science Applications,Mechanical Engineering,Mechanics of Materials
Reference8 articles.
1. Box, G. E. P, and Draper, N. R., 1987, Empirical Model Building and Response Surfaces, Wiley, New York. 2. Sobieszczansi-Sobieski, J., 1988, “Optimization by Decomposition: A Step from Hierarchic to Non-Hierarchic Systems,” NASA Conference Publication 3031, Part 1, Second NASA/Air Force Symposium on Recent Advances in Multidisciplinary Analysis and Optimization, Hampton, VA. 3. Renaud, J. E., and Gabriele, G. A., 1993, “Improved Coordination in Nonhierarchic System Optimization,” AIAA J., 31, No. 12, pp. 2367–2373. 4. Sellar, R. S., Batill, S. M., and Renaud, J. E., 1996, “Response Surface Based, Concurrent Subspace Optimization for Multidisciplinary Design,” AIAA Paper 96-0714, 34th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV. 5. Stelmack, M. A., Batill, S. M., Beck, B. C., and Flask, D. J., 1998, “Application of the Concurrent Subspace Design Framework to Aircraft Brake Component Design Optimization,” AIAA Paper 98-2033, 39th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Long Beach, CA.
Cited by
7 articles.
订阅此论文施引文献
订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献
|
|