Multidisciplinary optimization in aircraft design using analysis technology models
An approach to multidisciplinary optimization is presented which combines the Global Sensitivity Equation method, parametric optimization, and analytic technology models. The result is a powerful yet simple procedure for identifying key design issues. It can be used both to investigate technology in...
Main Author: | Malone, Brett |
---|---|
Other Authors: | Aerospace Engineering |
Format: | Others |
Language: | en |
Published: |
Virginia Tech
2014
|
Subjects: | |
Online Access: | http://hdl.handle.net/10919/45102 http://scholar.lib.vt.edu/theses/available/etd-10102009-020042/ |
Similar Items
-
Intersection and filleting of non-uniform B-spline surfaces
by: Jones, Robert W.
Published: (2014) -
Filleting of aircraft components using non-uniform B-spline surfaces
by: Gloudemans, James R.
Published: (2014) -
Control authority assessment in aircraft conceptual design
by: Kay, Jacob
Published: (2014) -
Interactive calculation of cross-sectional areas for aircraft design and analysis
by: Grieshaber, Michele Marie
Published: (2014) -
Rule-based fuselage and spine and cross-section methods for computer aided design of aircraft components
by: Kelly, John H.
Published: (2014)