Study on control of axisymmetric jet by half delta-wing shaped vortex generators (Part 2: Evaluation of statistics on the thermal field)
Author:
Affiliation:
1. Department of Mechanical Science and Engineering, Nagoya University
2. Department of Aerospace Engineering, Nagoya University
Publisher
Japan Society of Mechanical Engineers
Link
https://www.jstage.jst.go.jp/article/transjsme/82/838/82_16-00087/_pdf
Reference21 articles.
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2. Bradbury, L. J. S. and Khadem, A. H., The distortion of a jet by tabs, Journal of Fluid Mechanics, Vol.70 (1975), pp.801-813.
3. Enloe, C. L., McLaughlin, T. E., VanDyken, R. D., Kachner, K. D., Jumper, E. J., Corke, T. C., Post, M. and Haddad, O., Mechanisms and responses of a single dielectric barrier plasma actuator: geometric effects, AIAA Journal, Vol.42 (2004), pp.595-604.
4. Everson, R., Manin, D. and Sirovich, L., Quantification of mixing and mixing rate from experimental observations, AIAA Journal, Vol.36, No.2 (1998), pp.121-127.
5. Glezer, A. and Amitay, M., Synthetic jet, Annual Review of Fluid Mechanics, Vol.34 (2002), pp.503-529.
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