Experimental study of physical mechanisms in the control of supersonic impinging jets using microjets

DOI10.1017/S0022112008003091zbMath1151.76305OpenAlexW2026319572MaRDI QIDQ5302702

Rajan Kumar, Huadong Lou, Farrukh S. Alvi, Chiang Shih

Publication date: 8 January 2009

Published in: Journal of Fluid Mechanics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1017/s0022112008003091

Mathematics Subject Classification ID

Experimental work for problems pertaining to fluid mechanics (76-05) Supersonic flows (76J20) Flow control and optimization for compressible fluids and gas dynamics (76N25)

Related Items (1)

Axisymmetric jet manipulated using two unsteady minijets

Cites Work

• The effect of streamwise vortices on the aeroacoustics of a Mach 0.9 jet
• Mixing enhancement via nozzle trailing edge modifications in a high speed rectangular jet
• Mode-switching and nonlinear effects in compressible flow over a cavity
• Calculation of turbulence-driven secondary motion in non-circular ducts
• The two- and three-dimensional instabilities of a spatially periodic shear layer
• The instability of short waves on a vortex ring
• Spreading characteristics of compressible jets from nozzles of various geometries
• Three-dimensional instability and vorticity patterns in the wake of a flat plate
• On the use of microjets to suppress turbulence in a Mach 0.9 axisymmetric jet
• The near wall jet of a normally impinging, uniform, axisymmetric, supersonic jet
• Flow field and noise characteristics of a supersonic impinging jet
• An experimental study of the oscillatory flow structure of tone-producing supersonic impinging jets

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