Design and Analysis Integration Using Systems Engineering for Aircraft Structural Design-Reference-Cited by-同舟云学术

Design and Analysis Integration Using Systems Engineering for Aircraft Structural Design

Published:2004-06-19 Issue: Volume: Page:
ISSN:
Container-title:AIAA 4th Aviation Technology, Integration and Operations (ATIO) Forum
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Author:

Mawhinney Paul¹,Price Mark¹,Armstrong Cecil¹,Curran Richard¹,Early Juliana¹,Murphy Adrian¹,Benard Emmanuel¹,Raghunathan S.¹

Affiliation:

1. Queens University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2004-6204

Reference18 articles.

1. 1DefenseSystemsManagementCollege,andDefenseSystemsManagementCollege.Press,"Systemsengineering fundamentals,"Defense Systems Management College Press, Fort Belvoir,Va.;Washington, D.C.1999, pp.194.

2. 2Blair,J.C.,Ryan,R.S.,andSchutzenhofer,L.A."LaunchVehicleDesignProcess:Characterization,TechnicalIntegration, and Lessons Learned," NASA, TP-2001-210992,2001.

3. Constraint-based conceptual design and automated sensitivity analysis for airship concept studies

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