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Strength and Frequency of Underwater Shock Waves Related to Sterilization Effects on a Marine Bacterium Read chapter Read first chapter

2019 | OriginalPaper | Chapter

Review on Film Cooling in High-Speed Flows

Authors : K. Fujiwara, R. Sriram, K. Kontis, T. Ideta

Published in: 31st International Symposium on Shock Waves 2

Publisher: Springer International Publishing

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Abstract

This review presents the state of the art in film cooling applied to high-speed flows. Film cooling is a promising technique to reduce heat transfer and shield a surface that is exposed to high-temperature core stream. The technique applies cold pneumatic injection into a hot core stream, and while the film cooling in gas turbines is generally subsonic, it has also been a success in high-speed environment such as an extension nozzle of liquid rocket engines. The present paper aims to bring together the main results from experiments and numerical simulation on film cooling in high-speed flow. Parameters from not only fluid dynamical conditions but also gas properties and geometric features of injection affect the cooling performance.

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Literature
1.
2.
R.S. Bunker, A review of shaped hole turbine film cooling technology. J. Heat Transf. 127, 441–453 (2005)CrossRef
3.
R. Sriram, G. Jagadeesh, Film cooling at hypersonic Mach numbers using forward facing array of micro-jets. Int. J. Heat Mass Transf. 52, 3654–3664 (2009)CrossRef
4.
B.A. Haven, M. Kurosaka, Kidney and anti-kidney vortices in crossflow jets. J. Fluid Mech. 352, 27–64 (1997)CrossRef
5.
J.L. Stollery, A.A.M. El-Ehwany, A note on the use of a boundary-layer model for correlating film-cooling data. Int. J. Heat Mass Transf. 8, 55–65
6.
R.A. Seban, L.H. Back, Velocity and temperature profiles in turbulent boundary layers with tangential injection. J. Heat Transf. 84, 45–54 (1962)CrossRef
7.
R.J. Goldstein et al., Film cooling with air and helium injection through a rearward-facing slot into a supersonic air flow. AIAA J. 4(6), 981–985 (1966)CrossRef
8.
X. Yang et al., A numerical study of hypersonic laminar film cooling. Aeronaut. J., 479–486 (2003)
9.
K. Pathasarathy, V. Zakkay, An experimental investigation of turbulent slot injection at Mach 6. AIAA J. 8(7), 1302–1307 (1969)CrossRef
10.
R.W. Bass et al., Supersonic Film Cooling, AIAA second. Int. Aero. Planes Conf., 1–16 (1990)
11.
M. Hombsch, H. Oliver, Film cooling in laminar and turbulent supersonic flows. J. Spacecr. Rocket. 50(4), 742–753 (2013)CrossRef
12.
J.P. O’Connor, A. Haji-Sheikh, A Numerical Study of Film Cooling in Supersonic Flow, AIAA Paper (1991), AIAA-91-4010
13.
M. Keller, M.J. Kloker, Direct numerical simulations of film cooling in a supersonic boundary-layer flow on massively-parallel supercomputers, Sustained Simulation Performance (2013), pp. 107–128
14.
J. Linn, M.J. Kloker, Direct numerical simulation of film cooling in hypersonic boundary-layer flow, High Performance Computing in Science and Engineering, (2008), pp. 171–189
15.
M.A. Keller et al., Influence of cooling-gas properties on film-cooling effectiveness in supersonic flow. J. Spacecr. Rocket. 52(5), 1443–1455 (2015)CrossRef
16.
17.
T.F. Fric, A. Roshko, Vortical structure in the wake of a transverse jet. J. Fluid Mech. 279, 1–47 (1994)CrossRef
18.
A.R. Karagozian, Transverse jets and their control. Prog. Energy Combust. Sci. 36, 531–553 (2010)CrossRef
Metadata
Title
Review on Film Cooling in High-Speed Flows
Authors
K. Fujiwara
R. Sriram
K. Kontis
T. Ideta
Copyright Year
2019
Book
31st International Symposium on Shock Waves 2

Print ISBN: 978-3-319-91016-1

Electronic ISBN: 978-3-319-91017-8

Copyright Year: 2019

DOI
https://doi.org/10.1007/978-3-319-91017-8_118

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