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• W2188755892 abstract "Development of a MHz rate planar flow imaging system for real-time high-speed flow diagnostics is briefly described. The system has been utilized in supersonic jets with Mach numbers of 1.3 and 2.0 (convective Mach numbers of 0.59 and 0.85) to explore compressibility effects on large-scale turbulence structures. In addition to the loss of coherency due to compressibility, results show the convective velocity in the Mach 2.0 jet is bi-modal with a fast mode and a slow mode. The system has also been used in simultaneous flow imaging and acoustics measurements in a supersonic jet to explore sources of large peaks in the far acoustic field. The results have provided some new insight into the far-field acoustic waveform and the processes within the jet by which the peak acoustic radiation is generated." @default.
• W2188755892 created "2016-06-24" @default.
• W2188755892 creator A5015756609 @default.
• W2188755892 date "2002-01-01" @default.
• W2188755892 modified "2023-09-27" @default.
• W2188755892 title "Development and Application of Advanced Optical Diagnostics in High Speed Jets" @default.
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• W2188755892 hasPublicationYear "2002" @default.
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