A Weighted Nonlinear Filter Based High-order Finite Difference Scheme and Its Application to Supersonic Jet Flows (AIAA 2017-2243)
AIAA Interantional Space Planes and Hypersonic Systems and Technologies (Conference)
01.01.2017
12 pages
Aufsatz (Konferenz)
Englisch
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AIAA-2006-2243 Damage Characterization Through Nonlinear Analysis of Transient Vibrations
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