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Modeling and Simulation Techniques for the NASA SLS Service Module Panel Separation Event; From Loosely-Coupled Euler to Full-Coupled 6-DOF, Time-Accurate, Navier Stokes Methodologies
AIAA 2019-1843
Session: Special Session: Space Launch System Aerosciences I
Published Online:6 Jan 2019https://doi.org/10.2514/6.2019-1843