1999
DOI: 10.1002/(sici)1097-0363(19991215)31:7<1121::aid-fld913>3.0.co;2-r
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An adaptive least-squares method for the compressible Euler equations

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Cited by 17 publications
(3 citation statements)
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“…The reflected shock exits the domain from the top right corner which means that the shock reflection angle is captured very well, as shown in Figure 7. Figure 8 shows the pressure distribution for the current work against the work of Taghaddosi et al [30] Note that the results of Taghaddosi et al [30] are for inviscid flow. As shown in Figure 8, the pressure increases after passing the incident shock then increases again after the reflected shock.…”
Section: Viscous Shock Reflection (Vsr)mentioning
confidence: 79%
“…The reflected shock exits the domain from the top right corner which means that the shock reflection angle is captured very well, as shown in Figure 7. Figure 8 shows the pressure distribution for the current work against the work of Taghaddosi et al [30] Note that the results of Taghaddosi et al [30] are for inviscid flow. As shown in Figure 8, the pressure increases after passing the incident shock then increases again after the reflected shock.…”
Section: Viscous Shock Reflection (Vsr)mentioning
confidence: 79%
“…The non-conservative formulation of the Euler Equations were studied by Taghaddosi et al (1999) together with a grid adaptation method, where it was implemented a moving node strategy to obtain elements aligned with the shock. The slip boundary was implemented adding the boundary condition in the LSFEM functional.…”
Section: Lsfem Applied To the Euler Equationsmentioning
confidence: 99%
“…5.1. Taghaddosi et al (1999) and Pontaza et al (2004) also implemented the LSFEM applied to inviscid Euler Equations and simulated this problem.…”
Section: Shock Reflectionmentioning
confidence: 99%