Active Combustion Control Using a Fluidic Oscillator for Asymmetric Fuel Flow Modulation

By D. Guyot, Christian Oliver Paschereit, Surya Raghu. 2008

138 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Computational Mechanics, Fluid Flow and Transfer Processes

View Paper: https://www.semanticscholar.org/paper/271ed8253e410dc7a8a022b6fa77cbb7feb07221

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In Aerospace Engineering

1. Surya Raghu

In Computational Mechanics

1. Surya Raghu

In Fluid Flow and Transfer Processes

1. Surya Raghu

Citations in the corpus

• Performance Enhancement of a Vertical Tail Model with Sweeping Jet Actuators (2013, unknown): “In some of those designs [2 - 4] a wedge was placed in the center of the exit nozzle to ensure that the resulting oscillatory jet dwells at two prescribed angles.”
• Fluidic oscillators for flow control (2013, methodology): “Such pulsing diverters have been used in stator vane separation control (Culley et al. 2004) and in combustion NOx control (Guyot et al. 2008a, b, c).”