Derivation of Atmospheric Gust-Forcing Functions for Launch-Vehicle Loads Analysis
Author:
Affiliation:
1. The Aerospace Corporation, Los Angeles, California 90009-2957
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/2.3601
Reference36 articles.
1. Design and verification of launch and space vehicle structures
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3. Wind models for the NSTS ascent trajectory biasing for wind load alleviation
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3. Launch Vehicle Operational Environments;Encyclopedia of Aerospace Engineering;2010-12-15
4. Statistical Combination of Time-Varying Loads;AIAA Journal;2009-10
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