Open AccessA Mixed-Fidelity Approach for Design of Low-Boom Supersonic Aircraft
Author(s) -
Wu Li,
Elwood Shields,
Karl Geiselhart
Publication year - 2010
Publication title -
50th aiaa aerospace sciences meeting including the new horizons forum and aerospace exposition
Language(s) - English
Resource type - Conference proceedings
DOI - 10.2514/6.2010-845
Subject(s) - sonic boom , supersonic speed , boom , computational fluid dynamics , fuselage , aerospace engineering , marine engineering , computer science , engineering , environmental engineering
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