AIAA Propulsion and Energy 2019 Forum 2019
DOI: 10.2514/6.2019-4320
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Performance Enhancement of an External Compression Intake by the Boundary Layer Suction

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Cited by 2 publications
(2 citation statements)
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“…It is evident that a slot boundary layer bleed can significantly improve the intake performance and stability by preventing flow separation on the compression surface [58,91,108], especially when the shock train is close to the slot region [61,109]. Sethuraman et al [109] managed to reduce the shock oscillation by 50% with suction control, and reduced the oscillating frequency of the first shock by about 5 Hz, illustrating the effectiveness of the suction control when the shock train appears closer to the slot region [110].…”
Section: Boundary Layer Bleedmentioning
confidence: 99%
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“…It is evident that a slot boundary layer bleed can significantly improve the intake performance and stability by preventing flow separation on the compression surface [58,91,108], especially when the shock train is close to the slot region [61,109]. Sethuraman et al [109] managed to reduce the shock oscillation by 50% with suction control, and reduced the oscillating frequency of the first shock by about 5 Hz, illustrating the effectiveness of the suction control when the shock train appears closer to the slot region [110].…”
Section: Boundary Layer Bleedmentioning
confidence: 99%
“…Distortion in the intake flow of supersonic intake systems typically exhibits a complex spatial nature, coupled with significant temporal variability. Currently, there is a scarcity of research focused on total pressure distortion within unsteady supersonic intakes [90,108,232], clearly indicating that the AIP experiences a substantial increase in flow distortion when buzz occurs. A more substantial knowledge gap is discerned concerning the dynamic distortion experienced by unsteady supersonic intake systems.…”
Section: Current and Future Perspectives In Engine-intake Aerodynamic...mentioning
confidence: 99%