Time-Varying Structural Reliability of Launch Vehicle via Extreme Response Approach
Author:
Affiliation:
1. Sharif University of Technology, 11365-9567 Tehran, Iran
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.A33550
Reference24 articles.
1. Moving Aerospace Structural Design Practice to a Load and Resistance Factor Approach
2. Negative Stress Margins - Are They Real?
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5. Quadratic Limit States in Structural Reliability
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