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An investigation of the effective pressure ratio effects on the ejector-diffuser system

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References

  • Desevaux P, Bailly Y (2001) Numerical and experimental visualizations of the flow inside an induced air ejector. J Vis 4(4):311

    Article  Google Scholar 

  • Desevaux P, Mellal A, Alves de Sousa Y (2004) Visualization of secondary flow choking phenomena in a supersonic air ejector. J Vis 7(3):249–256

    Article  Google Scholar 

  • Katanoda H, Miyazato Y, Masuda M et al (2000) Pitot pressures of correctly-expanded and under expanded free jets from axisymmetric supersonic nozzles. Shock Waves 10(2):95–101

    Article  MATH  Google Scholar 

  • Kong FS, Kim HD, Jin Y et al (2013a) Application of chevron nozzle to a supersonic ejector–diffuser system. Procedia Eng 56:193–200

    Article  Google Scholar 

  • Kong F, Jin Y, Setoguchi T et al (2013b) Numerical analysis of Chevron nozzle effects on performance of the supersonic ejector-diffuser system. J Therm Sci 22(5):459–466

    Article  Google Scholar 

  • Mitchell DM, Honnery DR, Soria J (2012) The visualization of the acoustic feedback loop in impinging underexpanded supersonic jet flows using ultra-high frame rate schlieren. J Vis 15(4):333–341

    Article  Google Scholar 

  • Thiagarajan V, Panneerselvam S, Rathakrishnan E (2006) Numerical flow visualization of a Single Expansion Ramp Nozzle with hypersonic external flow. J Vis 9(1):91–99

    Article  Google Scholar 

  • Vishwanathappa MD (2005) Desalination of seawater using a high-efficiency jet ejector. Texas A&M University

  • Werle M, Presz WM Jr (2009) Shroud and ejector augmenters for subsonic propulsion and power systems. J Propul Power 25(1):228–236

    Article  Google Scholar 

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Acknowledgments

This work was supported by Advanced Research Center Program (No. 2013073861) through the National Research Foundation of Korea (NRF) grant funded by the Korea government (MSIP) contracted through Next Generation Space Propulsion Research Center at Seoul National University.

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Correspondence to Heuy Dong Kim.

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Kong, F., Kim, H.D. & Setoguchi, T. An investigation of the effective pressure ratio effects on the ejector-diffuser system. J Vis 18, 31–34 (2015). https://doi.org/10.1007/s12650-014-0235-0

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  • DOI: https://doi.org/10.1007/s12650-014-0235-0

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