A Multi-Fidelity Approach for Supporting Early Aircraft Design Decisions-Reference-Cited by-同舟云学术

A Multi-Fidelity Approach for Supporting Early Aircraft Design Decisions

Published: Issue: Volume: Page:267-279
ISSN:1865-5440
Container-title:Collaborative Product and Service Life Cycle Management for a Sustainable World
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Author:

Doherty John J,Dean Stephen R H,Ellsmore Paul,Eldridge Andrew

Publisher

Springer London

Link

http://link.springer.com/content/pdf/10.1007/978-1-84800-972-1_26.pdf

Reference13 articles.

1. ACARE, Strategic Research Agenda, Volumes 1 & 2, 2002. Available at: http://www.acare4europe.org. Accessed on: May 1st 2008.

2. Integrated Wing Aerospace Technology Validation Programme. Available at: https://www.integrated-wing.org.uk/default.htm. Accessed on: May 1st 2008.

3. ELLSMORE PD, RESTRICK KE. Application of RETIVO to Civil Aircraft. Paper AIAA-2007-7808, Belfast, 2007.

4. DOHERTY J, DEAN SRH. MDO-Based Concept Optimisation and The Impact of Technology and Systems Choices. Paper AIAA-2007-7806, 7th AIAA ATIO conference, Belfast, September 2007.

5. FENWICK SV, HARRIS JapC. The application of Pareto frontier methods in the multidisciplinary wing design of a generic modern military delta aircraft. In proceedings of NATO RTO AVT symposium, Ottawa, October 1999.

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