Reliability-based analysis and optimal design of an integral airframe structure lap joint-Reference-Cited by-同舟云学术

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Reliability-based analysis and optimal design of an integral airframe structure lap joint

Published:1999-04-12 Issue: Volume: Page:
ISSN:
Container-title:40th Structures, Structural Dynamics, and Materials Conference and Exhibit
language:
Short-container-title:

Author:

Fadale Tushar¹,Sues Robert¹

Affiliation:

1. Applied Research Associates, Inc., Raleigh, NC

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1999-1604

Reference9 articles.

1. NASA/CR 97-206284, 1997. 3. Gary, P. M., and Riskalla, M. G. "Development of

2. Elements for Aerospace Vehicle Structures, Volume I and 2, November 1, 1994. 6. Petit, R. G., Wang, J. J., and Toh, C. "Integral

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2. Fatigue reliability assessment of riveted lap joint of aircraft structures;International Journal of Fatigue;2012-10

3. Applications of Reliability Assessment;Engineering Design Reliability Handbook;2004-12-22

4. A Framework for Reliability-Based MDO of Aerospace Systems;43rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2002-04-22

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