The Influence of Rotation on the Internal Flow of a Cooled Turbine Blade With Serpentine-Shaped Cooling Channels

doi 10.1115/97-aa-115
Full Text
Abstract

Available in full text

Date
Authors
Publisher

American Society of Mechanical Engineers

Related search

Effect of Rotation on a Gas Turbine Blade Internal Cooling System: Experimental Investigation

2016English

Analysis on Gas Turbine Blade Cooling by Compressed Air Channels Using CFD Simulation

Asian Journal of Scientific Research
Multidisciplinary
2013English

The Solution-Adaptive Numerical Simulation of the 3D Viscous Flow in the Serpentine Coolant Passage of a Radial Inflow Turbine Blade

1992English

Design and Analysis of Gas Turbine Blade With Cooling

EAI Endorsed Transactions on Energy Web
ControlSystems EngineeringInformation SystemsEnergy EngineeringMarketingSustainabilityRenewable EnergyPower Technologythe Environment
2018English

Effect of Film-Cooling Hole Location on Turbulator Heat Transfer Enhancement in Turbine Blade Internal Air-Cooling Circuits

1999English

Numerical Analysis of Turbine Blade Cooling Ducts

Mathematical and Computer Modelling
2000English

Grid Generation and Fluid-Solid Coupling Methods for the Investigation of Gas Turbine Rotor Blade Internal Cooling

English

Impact of Surface Roughness on the Turbulent Wake Flow of a Turbine Blade

Journal of Aerodynamics
2014English

Numerical Investigation of Flow Around the Leading Edge of a Turbine Blade With Transpiration Cooling (1st Report, Properties for Fundamental Parameters)

Nihon Kikai Gakkai Ronbunshu, B Hen/Transactions of the Japan Society of Mechanical Engineers, Part B
Condensed Matter PhysicsMechanical Engineering
2003English

Amanote Research

Note-taking for researchers

Follow Amanote

© 2024 Amaplex Software S.P.R.L. All rights reserved.

Privacy PolicyRefund Policy