Computational prediction into staggered film cooling holes on convex surface of turbine blade
Author:
Publisher
Elsevier BV
Subject
Condensed Matter Physics,General Chemical Engineering,Atomic and Molecular Physics, and Optics
Reference27 articles.
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3. Computational study of film cooling from single and two staggered rows of novel semi-circular cooling holes including coolant plenum;Asghar;Energy Conversion and Management,2011
4. Film cooling effectiveness and net heat flux reduction of advanced cooling schemes using thermochromic liquid crystal;Ghorab;Applied Thermal Engineering,2011
5. Flow and heat transfer measurements of film injectant from a row of holes with compound angle orientations;Han;KSME International Journal,2002
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1. Experimental investigation and numerical analysis on effects of swirling coolant on flow characteristics and film cooling performance;International Communications in Heat and Mass Transfer;2022-06
2. Investigation and numerical simulation on film cooling performance with an anti-vortex hole design: Influences of diameter ratio;International Communications in Heat and Mass Transfer;2021-02
3. Film cooling performance evaluation of the furcate hole with cross-flow coolant injection: A comparative study;International Journal of Heat and Mass Transfer;2021-01
4. A computational study of mist assisted film cooling;International Communications in Heat and Mass Transfer;2018-07
5. Numerical Simulation on the Effect of Cooling Hole Configuration on the Film Cooling Effectiveness in TBC Coated Turbine Vanes;International Journal of Turbo & Jet-Engines;2018-03-30
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