Numerical Modeling of Transpiration-Cooled Turbulent Channel Flow with Comparisons to Experimental Data
Author:
Affiliation:
1. DLR, German Aerospace Center, 70569 Stuttgart, Germany
2. University of Stuttgart, 70569 Stuttgart, Germany
3. University of Sydney, Sydney, New South Wales 2006, Australia
Funder
Deutsche Forschungsgemeinschaft
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Condensed Matter Physics,Aerospace Engineering,Space and Planetary Science,Fluid Flow and Transfer Processes,Mechanical Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.T5266
Reference35 articles.
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2. Effect of fluid-thermal–structural interactions on the topology optimization of a hypersonic transport aircraft wing
3. EckertE.LivingoodJ. “Comparison of Effectiveness of Convection- Transpiration- and Film Cooling Methods with Air as a Coolant,” NACA TR1182, 1955.
4. A comparison between film cooling and transpiration cooling systems in high speed flow
5. L’EcuyerM.CollodayR. “Influence of Porous-Wall Thermal Effectiveness on Turbulent-Boundary-Layer Heat Transfer,” NASA Lewis Research Center TN D-6837, Cleveland, OH, 1972.
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