Supersonic Turbulent Flow Modelling Over Steps And Cavities

Altitude compensating nozzles provide ideal conditions for propulsion, ignoring the effect of atmospheric pressure that will cause the reduction of efficiency. Past experiments discovered the effect of fuel combustion on the surface of nozzles, which causes cross-hatching patterns on the wall due to...

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Bibliographic Details
Main Author: Lee, Kah Kheng
Format: Monograph
Language:English
Published: Universiti Sains Malaysia 2021
Subjects:
Online Access:http://eprints.usm.my/54534/1/Supersonic%20Turbulent%20Flow%20Modelling%20Over%20Steps%20And%20Cavities.pdf
http://eprints.usm.my/54534/
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