2014
DOI: 10.6112/kscfe.2014.19.4.014
|View full text |Cite
|
Sign up to set email alerts
|

Design Optimization and Performance Analysis of Internal Cooling Passage With Various Type of Rib Turbulator for High Pressure Turbine Nozzle

Abstract: This study conducts shape optimization of rib turbulator on the internal cooling passage that has triangular cross-section of high pressure turbine nozzle. During optimization, various types of rib turbulator including angled, V-shaped

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...

Citation Types

0
0
0

Publication Types

Select...

Relationship

0
0

Authors

Journals

citations
Cited by 0 publications
references
References 8 publications
0
0
0
Order By: Relevance

No citations

Set email alert for when this publication receives citations?