Free-Stream Turbulence Effects on Film Cooling With Shaped Holes
By C. Saumweber, A. Schulz, S. Wittig. 2002
239 citations recorded by the source corpus.
Subfields: Aerospace Engineering, Computational Mechanics, Mechanical Engineering
View Paper: https://www.semanticscholar.org/paper/74da9e43505192353b9d4e355111a290fe5725a5
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In Aerospace Engineering
In Computational Mechanics
In Mechanical Engineering
Citations in the corpus
- ADIABATIC EFFECTIVENESS MEASUREMENTS FOR A BASELINE SHAPED FILM COOLING HOLE (2014, background): “Overall the design choices differentiated the 7-7-7 baseline shaped hole from the geometry investigated extensively by Wittig and coworkers [26, 32, 34-37].”
- Optimization of a Cylindrical Film Cooling Hole using Surrogate Modeling (2009, background): “[1] for the same conditions (L=D1⁄4 6.”
- Shape optimization of a fan-shaped hole to enhance film-cooling effectiveness (2010, background): “[3] studied the variation of the film-cooling performance with the turbulence intensity of the free-stream and the ejection angle for cylindrical and two different-shaped holes.”