Validation of an Output-Adaptive, Tetrahedral Cut-Cell Method for Sonic Boom Prediction
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Virgnia 23681
2. Massachusetts Institute of Technology, Cambridge, Massachusetts 02139
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J050111
Reference67 articles.
1. State of the art of sonic boom modeling
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1. Recent Enhancements to Modeling Sonic Boom Propagation using Augmented Burgers' Equation;AIAA AVIATION 2023 Forum;2023-06-08
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3. Numerical Simulations of a Quiet SuperSonic Technology (QueSST) Aircraft Preliminary Design;2018 Fluid Dynamics Conference;2018-06-24
4. Adjoint-Based Mesh Adaptation for the Sonic Boom Signature Loudness;35th AIAA Applied Aerodynamics Conference;2017-06-02
5. Full-Field Sonic Boom Simulation in Stratified Atmosphere;AIAA Journal;2016-10
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