Elastic Launch Vehicle Response to Sinusoidal Gusts
Author:
Affiliation:
1. Lockheed Missiles & Space Company Inc., Sunnyvale, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.61874
Reference23 articles.
1. Progress on the launch-vehicle buffeting problem
2. Analysis of flow separation effects on the dynamics of a large space booster
3. Determination of launch-vehicle response to detailed wind profiles
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