DTIC ADA586719: High Order Accuracy Methods for PDEs with Shocks an... | |
by Defense Technical Information Center | |
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The aim of this project is the construction of efficient | |
high fidelity schemes for systems of PDEs that contain | |
shock waves. We advocate here the Discontinuous | |
collocation method, i.e. multi-domain spectral method | |
with stable and conservative penalty interface | |
conditions. In this work, the previously developed | |
methodology is generalized to inhomogeneous grid to | |
simulate the two dimensional supersonic injector-cavity | |
system. Non-physical modes generated at the domain | |
interfaces due to the spatial grid inhomogeneity is | |
minimized using the new weighted multi-domain spectral | |
penalty method. The method yields accurate and stable | |
solutions of the injector-cavity system which agree well | |
with experiments qualitatively. Through the direct | |
numerical simulation of the injector-cavity system using | |
the weighted method, the geometric effect of the cavity | |
wall on the pressure fluctuation is investigated. It is | |
shown that the recessed slanted cavity attenuates | |
pressure fluctuations inside cavity enabling the cavity | |
to act potentially as a stable flameholder for scramjet | |
engine. | |
Date Published: 2018-09-15 16:06:09 | |
Identifier: DTIC_ADA586719 | |
Item Size: 8403292 | |
Language: english | |
Media Type: texts | |
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DTIC Archive; ; BROWN UNIV PROVIDENCE... | |
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@chris85 | |
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