What is it about?
A unique case allowing to evaluate the strength and limitations of an Euler solver by computing the aerodynamics of a reentry vehicle within a full range of Mach numbers (0.3 to 20.0)
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Why is it important?
Assess the computational method strength and limitations, establish confidence
Perspectives
This study also incorporates educational value
Dr. Dan Almosnino
Independent Consultant
Read the Original
This page is a summary of: Assessment of an Inviscid Euler-Adjoint Solver for Prediction of Aerodynamic Characteristics of the NASA HL-20 Lifting Body, June 2016, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/6.2016-3266.
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