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Advanced Design Methodology for Robust Aircraft Sizing and SynthesisContract efforts are focused on refining the Robust Design Methodology for Conceptual Aircraft Design. Robust Design Simulation (RDS) was developed earlier as a potential solution to the need to do rapid trade-offs while accounting for risk, conflict, and uncertainty. The core of the simulation revolved around Response Surface Equations as approximations of bounded design spaces. An ongoing investigation is concerned with the advantages of using Neural Networks in conceptual design. Thought was also given to the development of systematic way to choose or create a baseline configuration based on specific mission requirements. Expert system was developed, which selects aerodynamics, performance and weights model from several configurations based on the user's mission requirements for subsonic civil transport. The research has also resulted in a step-by-step illustration on how to use the AMV method for distribution generation and the search for robust design solutions to multivariate constrained problems.
Document ID
19980200851
Acquisition Source
Langley Research Center
Document Type
Contractor Report (CR)
Authors
Mavris, Dimitri N.
(Georgia Inst. of Tech. Atlanta, GA United States)
Date Acquired
September 6, 2013
Publication Date
November 11, 1997
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA/CR-97-206119
NAS 1.26:206119
Report Number: NASA/CR-97-206119
Report Number: NAS 1.26:206119
Funding Number(s)
CONTRACT_GRANT: NAG1-1793
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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