Inverse estimation of inlet parameters in an axisymmetric cylindrical combustor with thermal radiation effect
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Publication:656746
DOI10.1016/j.ijheatmasstransfer.2011.08.004zbMath1243.80007OpenAlexW2066798696MaRDI QIDQ656746
Publication date: 13 January 2012
Published in: International Journal of Heat and Mass Transfer (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1016/j.ijheatmasstransfer.2011.08.004
thermal radiationinverse analysismass fractiondiffusion-controlled turbulent combustioninlet velocityrepulsive particle swarm optimization
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Cites Work
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- Numerical investigation of combustion with non-gray thermal radiation and soot formation effect in a liquid rocket engine
- Inverse radiation analysis using repulsive particle swarm optimization algorithm
- Inverse estimation of inlet parameters in diffusion-controlled turbulent combustion in an axisymmetric combustor
- Numerical study on supersonic combustion with cavity-based fuel injection
- A CONTROL VOLUME FINITE-ELEMENT METHOD FOR TWO-DIMENSIONAL FLUID FLOW AND HEAT TRANSFER
- SOLUTION OF SOME TWO-DIMENSIONAL INCOMPRESSIBLE FLOW PROBLEMS USING A CURVILINEAR COORDINATE SYSTEM BASED CALCULATION PROCEDURE
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