Cover image for Numerical analysis of film cooling effectiveness using compound cooling holes at the end of gas turbine engine combustor
Title:
Numerical analysis of film cooling effectiveness using compound cooling holes at the end of gas turbine engine combustor
Personal Author:
Publication Information:
2014
Physical Description:
xvii, 140 p. : ill. ; 30 cm
General Note:
Supervisor : Dr. Nor Azwadi Che Sidik

Also available in CD-ROM : CP 050625 ra
Added Author:
Added Corporate Author:
DSP_DISSERTATION:
Thesis (Sarjana Kejuruteraan (Mekanikal)) - Universiti Teknologi Malaysia, 2014

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32000000000905 TL701.5 S53 2014 raf Closed Access Thesis UTM Master Thesis (Closed Access)
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30000010330064 TL701.5 S53 2014 raf Closed Access Thesis UTM Master Thesis (Closed Access)
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