In-tube shock wave compression by piston effect of unsteady jet

Author:

KUWABARA Daisuke1,KAWASAKI Hirokatsu12,IWAKAWA Akira13,SASOH Akihiro1,YAMASHITA Tetsuya4,TAGUCHI Koji4

Affiliation:

1. Department of Aerospace Engineering, Nagoya University

2. Currently, Kawasaki Heavy Industries, Ltd.

3. Currently, DENSO CORPORATION

4. US URASAKI Co., Ltd

Publisher

Japan Society of Mechanical Engineers

Subject

General Medicine

Reference15 articles.

1. Arakeri J. H., Das D., Krothapalli A. and Lourenco L., Vortex ring formation at the open end of a shock tube: A particle image velocimetry study, Physics of Fluids, Vol.16 (2004), pp.1008-1019.

2. Ascher H. Shapiro, The Dynamics and Thermodynamics of Compressible Fluid Flow, Vol.Ⅱ (1954), pp.1007, 1014.

3. Brocher E., C. Maresca and M.-H. Bournay, Fluid dynamics of the resonance tube, J. Fluid Mech, Vol.43, part.2 (1970), pp.369-384.

4. Ganesh Raman and K. Srinivasan, The powered resonance tube: From Hartmann’s discovery to current active flow control applications, Progress in Aerospace Sciences, Vol.45 (2009), pp.97-123.

5. George Rundinger, On the Reflection of Shock Waves from an Open End of a Duct, Journal of Applied Physics, Vol.26, No.8 (1955), pp.980-993.

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