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Drozda, T.G., Baurle, R.A. and Drummond, J.P. (2016) Impact of Flight Enthalpy, Fuel Stimulant, and Chemical Reactions on the Mixing Characteristics of Several Injectors at Hypervelocity Flow Conditions. NASA Langley Research Center, Hampton, VA, Document ID: 20160009131.
https://ntrs.nasa.gov/api/citations/20160009131/downloads/20160009131.pdf

has been cited by the following article:

• TITLE: Liquid Jet Blasting Using Ultra-High Frequency Supersonic Pulsed Air Jet

  AUTHORS: John T. Solomon

  KEYWORDS: Ultrasonic Actuators, Flow Control, Liquid Blasting

  JOURNAL NAME: Journal of Flow Control, Measurement & Visualization, Vol.10 No.2, April 11, 2022

  ABSTRACT: This paper reports an experimental study on a liquid injector assembly integrated with an ultra-high frequency pulsed air jet that operates at 21 kHz. The active air-blasting assembly steadily injects a liquid through four micro-nozzles of 0.4 mm diameters each, positioned around a 1 mm nozzle through which the pulsed actuation jet flows out at supersonic velocity. High-frequency compressible air vortexes and shock waves generated by the injector atomize the liquid stream into finer droplets and distribute them to a larger area to improve mixing with the ambiance. The paper presents the design details and preliminary studies on the flow field characteristics of this novel injection scheme, which is a potential candidate for high-speed flow mixing and control applications.