Flowfield measurements in supersonic film cooling including the effect of shock-wave interaction

Conference proceeding

Peer reviewed

K. A Juhany and M. L Hunt

AIAA journal, Vol.32(3), pp.578-585

01/03/1994

Abstract

Applied sciences

Combustion of gaseous fuels

Combustion. Flame

Compressible flows; shock and detonation phenomena

Energy

Energy. Thermal use of fuels

Exact sciences and technology

Fluid dynamics

Fundamental areas of phenomenology (including applications)

Physics

Shock-wave interactions and shock effects

Shock-wave interactions and shockeffects

Theoretical studies. Data and constants. Metering

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Title: Flowfield measurements in supersonic film cooling including the effect of shock-wave interaction
Creators - without role: K. A Juhany - California Institute of Technology
M. L Hunt - California Institute of Technology
Publication Details: AIAA journal, Vol.32(3), pp.578-585
Publisher: American Institute of Aeronautics and Astronautics
Identifiers: 9938570708331
Academic Unit: King Abdulaziz University
Language: English
Resource Type: Conference proceeding