2019
DOI: 10.1016/j.actaastro.2019.02.008
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Performance assessment of supersonic and hypersonic intake systems with nano-particle injection

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Cited by 6 publications
(1 citation statement)
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“…Table 2 illustrates the three different flow control methods (boundary layer porous bleed, VGs, and mass injection using a plasma jet example) discussed in this section, implemented on shock-dominated flows. Jagannathan et al [142] numerically investigated the effect of boron particle injection on a 2D rectangular-mixed compression intake at M ∞ = 3.0. For simplification, the study ignored shockwave-boundary layer-particle interactions and other viscous effects and achieved about a 16% increase in the intake pressure recovery due to the momentum and energy transfer effects of the nanoaerosol.…”
Section: Mass Injection and Energy Depositionmentioning
confidence: 99%
“…Table 2 illustrates the three different flow control methods (boundary layer porous bleed, VGs, and mass injection using a plasma jet example) discussed in this section, implemented on shock-dominated flows. Jagannathan et al [142] numerically investigated the effect of boron particle injection on a 2D rectangular-mixed compression intake at M ∞ = 3.0. For simplification, the study ignored shockwave-boundary layer-particle interactions and other viscous effects and achieved about a 16% increase in the intake pressure recovery due to the momentum and energy transfer effects of the nanoaerosol.…”
Section: Mass Injection and Energy Depositionmentioning
confidence: 99%