Momentum Diffusion Near Jet Exit in a Round Jet Controlled by Half Delta-Wing Tabs-Reference-Cited by-同舟云学术

Momentum Diffusion Near Jet Exit in a Round Jet Controlled by Half Delta-Wing Tabs

Published:2020-04-10 Issue:3 Volume:105 Page:715-734
ISSN:1386-6184
Container-title:Flow, Turbulence and Combustion
language:en
Short-container-title:Flow Turbulence Combust

Author:

Ito Yasumasa,Naganawa Kosuke,Sakai Yasuhiko,Iwano Koji

Funder

Kakenhi

Publisher

Springer Science and Business Media LLC

Subject

Physical and Theoretical Chemistry,General Physics and Astronomy,General Chemical Engineering

Link

https://link.springer.com/content/pdf/10.1007/s10494-020-00129-x.pdf

Reference29 articles.

1. Bradbury, L.J.S., Khadem, A.H.: The distortion of a jet by tabs. J. Fluid Mech. 70, 801–813 (1975)

2. Carletti, M.J., Rogers, C.B., Parekh, D.E.: Parametric study of jet mixing enhancement by vortex generators, tabs, and deflector plates. ASME Mech. Eng. Fluids Eng. Div. Conf. 237, 303–312 (1996)

3. Fernando, F.G.: Vortex dynamics and entrainment in rectangular free jets. J. Fluid Mech. 437, 69–101 (2001)

4. Heeb, N., Gutmark, E., Kailasanath, K.: An experimental investigation of the flow dynamics of streamwise vortices of various strengths interacting with a supersonic jet. Phys. Fluids 26, 086102 (2014)

5. Heeb, N., Gutmark, E., Kailasanath, K.: Impact of chevron spacing and asymmetric distribution on supersonic jet acoustics and flow. J. Sound Vib. 370, 54–81 (2016)

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