Skip to content
VuFind
English
Deutsch
Español
Français
Italiano
日本語
Nederlands
Português
Português (Brasil)
中文(简体)
中文(繁體)
Türkçe
עברית
Gaeilge
Cymraeg
Ελληνικά
Català
Euskara
Русский
Čeština
Suomi
Svenska
polski
Dansk
slovenščina
اللغة العربية
বাংলা
Galego
Tiếng Việt
Hrvatski
हिंदी
Հայերէն
Українська
Sámegiella
Монгол
Language
All Fields
Title
Author
Subject
Call Number
ISBN/ISSN
Tag
Find
Advanced
The effect of injection angle...
Cite this
Text this
Email this
Print
Export Record
Export to RefWorks
Export to EndNoteWeb
Export to EndNote
Permanent link
The effect of injection angle on the suction side of a turbine blade in film cooling system /
20
Bibliographic Details
Main Authors:
177619 Mohd. Nor Musa
,
Rosli Abu Bakar
,
Aminudin Abu
,
Kongres Sains dan Teknologi Malaysia (1994 : Kuala Lumpur)
Format:
Subjects:
Cooling systems
Gas-turbines
Holdings
Description
Similar Items
Staff View
Similar Items
Advanced gas turbine cooling: double-wall turbine cooling technologies in turbine NGV/blade applications
by: Murray, AV
Published: (2019)
Internal cooling for HP turbine blades
by: Pearce, R
Published: (2016)
Review of Research on Swirl Cooling Technology of Gas Turbine Blades
by: ZUO Qiuru, et al.
Published: (2024-10-01)
The cooling performance of three-row compound angle holes on the suction surface of a rotating turbine blade
by: Zhiyu Zhou, et al.
Published: (2021-03-01)
The Effects of Inclination and Compounds Angles of Round Holes in Staggered Rows on Adiabatic Film Cooling Effectiveness of Vane Suction side
by: Najdat N. Abdullah, Prof. Dr., et al.
Published: (2016-06-01)