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Studies of Shock Wave Reflections and Interactions (Paul Vieille Lecture) Read chapter Read first chapter

2017 | OriginalPaper | Chapter

Mixing Enhancement in Free Jets from Supersonic ESTS Lobed Nozzles

Authors : Albin Varghese, S. K. Karthick, Srisha M. V. Rao, Gopalan Jagadeesh

Published in: 30th International Symposium on Shock Waves 1

Publisher: Springer International Publishing

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Abstract

Mixing enhancement of two gaseous streams at high Mach numbers plays an important role in the design of supersonic ejectors and supersonic combustors. In order to obtain mixing enhancements in supersonic jets, many nozzles with exotic shapes have been developed [1].

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previous chapter Effect of the Adiabatic Index on the Shock Reflection in Overexpanded Nozzle Flow
next chapter Study of Cluster Linear Plug Nozzle Flow Field in Freestream Flow
Literature
1.
Papamoschou, D., Roshko, A.: The compressible turbulent shear layer: an experimental study. J. Fluid Mech. 197, 453477 (1988)CrossRef
2.
Gutmark, E., Schadow, K., Yu, K.: Mixing enhancement in supersonic free shear flows. Annu. Rev. Fluid Mech. 27, 375417 (1995)CrossRef
3.
Rao, S.: Experimental investigations on supersonic ejectors. PhD thesis, Aerospace Engineering, Indian Institute of Science, Bangalore (2013)
4.
Rao, S., Jagadeesh, G.: Novel supersonic nozzles for mixing enhancement in supersonic ejectors. Appl. Therm. Eng. 71(1), 6271 (2014)CrossRef
5.
Clemens, N., Mungal, M.: A planar Mie scattering technique for visualizing supersonic mixing flows. Exp. Fluid 11(1), 175185 (1991)
Metadata
Title
Mixing Enhancement in Free Jets from Supersonic ESTS Lobed Nozzles
Authors
Albin Varghese
S. K. Karthick
Srisha M. V. Rao
Gopalan Jagadeesh
Copyright Year
2017
Book
30th International Symposium on Shock Waves 1

Print ISBN: 978-3-319-46211-0

Electronic ISBN: 978-3-319-46213-4

Copyright Year: 2017

DOI
https://doi.org/10.1007/978-3-319-46213-4_15

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