Analysis of Ares Crew Launch Vehicle Transonic Alternating Flow Phenomenon
Author:
Affiliation:
1. NASA Langley Research Center, 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.A32154
Reference9 articles.
1. PRESSURE FLUCTUATIONS RESULTING FROM AN ALTERNATING FLOW SEPARATION AND ATTACHMENT AT TRANSONIC SPEEDS
2. Progress on the launch-vehicle buffeting problem
3. Vibration response of spacecraft shrouds toin-flight fluctuating pressures
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