Volume 2D: Turbomachinery 2016
DOI: 10.1115/gt2016-56647
|View full text |Cite
|
Sign up to set email alerts
|

Numerical Study on the Effects of the Upstream Wake Generator on the Aerodynamic Performance of a High-Lift Low Pressure Turbine Blade

Abstract: The aim of the present paper is to analyze and discuss in detail the effects of the upstream incoming wakes on both the aerodynamic loading and the evolution of the laminar separation bubble developing along the suction side of the high-lift T106-C low pressure turbine blade at engine similar Reynolds and Mach numbers, but at a low free stream turbulence level. The investigation is carried out numerically by means of steady and unsteady RANS simulations for two different Reynolds numbers (100,000 and 140,000),… Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
1

Citation Types

0
1
0

Year Published

2017
2017
2017
2017

Publication Types

Select...
1

Relationship

0
1

Authors

Journals

citations
Cited by 1 publication
(1 citation statement)
references
References 0 publications
0
1
0
Order By: Relevance
“…The unsteady interaction between upstream wakes and the suction surface boundary layer of LPT blades has been studied by many researchers. [6][7][8] Hodson and Dawes 9 identified the wake-boundary layer interaction in LPTs and found that the upstream wakes reduced the profile losses by suppressing the blade surface boundary layer separation, which changed the traditional understanding that wakes increased the flow turbulence and resulted in increased profile losses. Curtis et al 10 found that unsteady wakes contributed to the transition of blade surface boundary layers.…”
Section: Introductionmentioning
confidence: 99%
“…The unsteady interaction between upstream wakes and the suction surface boundary layer of LPT blades has been studied by many researchers. [6][7][8] Hodson and Dawes 9 identified the wake-boundary layer interaction in LPTs and found that the upstream wakes reduced the profile losses by suppressing the blade surface boundary layer separation, which changed the traditional understanding that wakes increased the flow turbulence and resulted in increased profile losses. Curtis et al 10 found that unsteady wakes contributed to the transition of blade surface boundary layers.…”
Section: Introductionmentioning
confidence: 99%