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Multidisciplinary Design Optimization for Aeropropulsion Engines and Solid Modeling/Animation via the Integrated Forced MethodsThe grant closure report is organized in the following four chapters: Chapter describes the two research areas Design optimization and Solid mechanics. Ten journal publications are listed in the second chapter. Five highlights is the subject matter of chapter three. CHAPTER 1. The Design Optimization Test Bed CometBoards. CHAPTER 2. Solid Mechanics: Integrated Force Method of Analysis. CHAPTER 3. Five Highlights: Neural Network and Regression Methods Demonstrated in the Design Optimization of a Subsonic Aircraft. Neural Network and Regression Soft Model Extended for PX-300 Aircraft Engine. Engine with Regression and Neural Network Approximators Designed. Cascade Optimization Strategy with Neural network and Regression Approximations Demonstrated on a Preliminary Aircraft Engine Design. Neural Network and Regression Approximations Used in Aircraft Design.
Document ID
20040084442
Acquisition Source
Glenn Research Center
Document Type
Other
Date Acquired
September 7, 2013
Publication Date
January 1, 2004
Subject Category
Aircraft Propulsion And Power
Funding Number(s)
CONTRACT_GRANT: NCC3-453
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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