What is it about?
Euler solver can become difficult at low Mach numbers due to equation-stiffness issues. This study assesses how well does the Cart3D/Adjoint Euler solver handle a complex configuration at low Mach number (M=0.3) and what are the limitations of the method
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Why is it important?
The case helps to build confidence in the solution method as well as understand its limitations.
Perspectives
The study also contributes educational value.
Dr. Dan Almosnino
Independent Consultant
Read the Original
This page is a summary of: A Low Subsonic Study of the NASA N2A Hybrid Wing-Body Using an Inviscid Euler-Adjoint Solver, June 2016, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/6.2016-3267.
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