2016
DOI: 10.1007/s00348-016-2145-5
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Experimental characterization of turbulent subsonic transitional–open cavity flow

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Cited by 7 publications
(2 citation statements)
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“…Increasing the Mach number showed a subtle effect on the store forces and moments for closed cavity flows while significantly reducing the pitching moment for transitional cavity flows. Despite the accumulation of a substantial volume of experimental data over the years, conducting wind tunnel experiments of cavities with stores remains a formidable challenge [31,32]. Even non-intrusive techniques, such as particle image velocimetry (PIV) and pressure-sensitive paint (PSP), which offer high spatial and temporal resolutions [33][34][35], encounter limitations in applications involving relatively complex cavity geometries at high-Reynolds and high-Mach flows due to their intricate setups.…”
Section: Introductionmentioning
confidence: 99%
“…Increasing the Mach number showed a subtle effect on the store forces and moments for closed cavity flows while significantly reducing the pitching moment for transitional cavity flows. Despite the accumulation of a substantial volume of experimental data over the years, conducting wind tunnel experiments of cavities with stores remains a formidable challenge [31,32]. Even non-intrusive techniques, such as particle image velocimetry (PIV) and pressure-sensitive paint (PSP), which offer high spatial and temporal resolutions [33][34][35], encounter limitations in applications involving relatively complex cavity geometries at high-Reynolds and high-Mach flows due to their intricate setups.…”
Section: Introductionmentioning
confidence: 99%
“…C AVITY flow is a ubiquitous aerodynamic configuration with applications ranging from aircraft landing gear bays and cargo/ weapons bays to flameholding in scramjets and flow regimes from low subsonic to supersonic [1][2][3][4][5]. Cavity flows often resonate, potentially causing serious aerodynamic repercussions [1,5].…”
Section: Introductionmentioning
confidence: 99%