Influence of injectant mach number and temperature on supersonic film cooling

Journal article

Peer reviewed

K. A Juhany, M. L Hunt and J. M Sivo

Journal of thermophysics and heat transfer, Vol.8(1), pp.59-67

1994

Abstract

Applied sciences

Continuous cycle engines: steam and gas turbines, jet engines

Engines and turbines

Exact sciences and technology

Mechanical engineering. Machine design

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Title: Influence of injectant mach number and temperature on supersonic film cooling
Creators - without role: K. A Juhany - California Institute of Technology
M. L Hunt - California Institute of Technology
J. M Sivo - California Institute of Technology
Publication Details: Journal of thermophysics and heat transfer, Vol.8(1), pp.59-67
Publisher: American Institute of Aeronautics and Astronautics
Identifiers: 9938402108331
Academic Unit: King Abdulaziz University
Language: English
Resource Type: Journal article