Computational Aeroelastic Analysis of the Ares I Crew Launch Vehicle During Ascent
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Virginia 23681
2. ATK Aerospace Company, Hampton, Virginia 23681
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.A32127
Reference33 articles.
1. Aeroelastic Vehicle Dynamics of a Proposed Delta II 7920-10L Launch Vehicle
2. Aeroelastic instability caused by slender payloads.
3. Unsteady Flow Separation Can Endanger the Structural Integrity of Aerospace Launch Vehicles
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