Publication Date:
2019-07-13
Description:
Linearized Euler equations are used to simulate supersonic jet noise generation and propagation. Special attention is given to boundary treatment. The resulting solution is stable and nearly free from boundary reflections without the need for artificial dissipation, filtering, or a sponge layer. The computed solution is in good agreement with theory and observation and is much less CPU-intensive as compared to large-eddy simulations.
Keywords:
Fluid Mechanics and Heat Transfer
Type:
NASA-TM-106929
,
ICOMP-95-9
,
E-9650
,
NAS 1.15:106929
,
AIAA Paper 95-0505
,
33rd Aerospace Sciences Meeting and Exhibit; Jan 09, 1995 - Jan 12, 1995; Reno, NV; United States
Format:
application/pdf
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