Amanote Research

Amanote Research

    RegisterSign In

Experimental and Numerical Studies on Leading Edge Film Cooling Performance: Effects of Hole Exit Shape and Freestream Turbulence

doi 10.1115/gt2012-68217
Full Text
Open PDF
Abstract

Available in full text

Date

June 11, 2012

Authors
Ken-ichi FunazakiHirokazu KawabataDaichi TakahashiYoji Okita
Publisher

American Society of Mechanical Engineers


Related search

The Effect of High Freestream Turbulence on Film Cooling Effectiveness

1994English

Showerhead Film Cooling Performance of a Turbine Vane at High Freestream Turbulence in a Transonic Cascade

Journal of Turbomachinery
Mechanical Engineering
2012English

Effect of Hole Configurations on Film Cooling Performance

Numerical Heat Transfer; Part A: Applications
Numerical AnalysisCondensed Matter Physics
2019English

Effects of Free-Stream Turbulence and Surface Roughness on Film Cooling

1996English

Effect of Velocity and Temperature Distribution at the Hole Exit on Film Cooling of Turbine Blades

1995English

Effects of Flow Compressibility and Density Ratio on Film Cooling Performance

Journal of Propulsion and Power
SpacePlanetary ScienceFuel TechnologyMechanical EngineeringAerospace Engineering
2017English

Effects of Hub Endwall Geometry and Rotor Leading Edge Shape on Performance of Supersonic Axial Impulse Turbine. Part I

2017English

Experimental Studies of Film Cooling in Supersonic Combustors

2017English

Numerical and Experimental Investigation of the Methane Film Cooling in Subscale Combustion Chamber

2016English

Amanote Research

Note-taking for researchers

Follow Amanote

© 2025 Amaplex Software S.P.R.L. All rights reserved.

Privacy PolicyRefund Policy