Improved MSMGFSK Models Apply to Gas Radiation Heat Transfer Calculation of Exhaust System of TBCC

2016 ◽  
Vol 139 (1) ◽  
Author(s):  
Haiyang Hu ◽  
Qiang Wang

The multiscale multigroup full-spectrum k-distribution (MSMGFSK) model was improved to adapt to radiation heat transfer calculations of combustion gas flow field with large temperature and pressure gradient. The improvements in calculation accuracy resulting from new sorting strategy of the spectral absorption coefficients were validated using a series of semi-1D problem in which strong temperature, pressure, and mole fraction inhomogeneities were present. A simpler method to attain compatibility between the MSMGFSK model and the gray-wall radiation emission has been established and validated. Finally, estimates are given for the calculation of wall radiation heat transfer characteristics and thermal emission imaging of the exhaust system of the parallel turbine-based combined cycle (TBCC) engine, using finite volume method (FVM) and ray trace method (RT), respectively.

2017 ◽  
Vol 140 (3) ◽  
Author(s):  
Yue Zhou ◽  
Qiang Wang ◽  
Haiyang Hu

In the present work, strategies for the grouping of the spectral absorption coefficients used in multiscale (MS) multigroup (MG) full-spectrum k-distribution models were improved by considering the effects of variations in both temperature and species molar ratio on the correlated-k characteristics of the spectra of H2O–CO2-soot mixtures. The improvements in the accuracy of predictions of radiation heat transfer characteristics resulting from these new grouping strategies were evaluated using a series of semi-one-dimensional (1D) cases with significant temperature, participating species molar ratio, and pressure inhomogeneities. Finally, evaluations of grouping strategies were presented on calculation of the full-spectrum thermal images of an actual aeroengine combustor.


2000 ◽  
Author(s):  
B. Golchert ◽  
C. Q. Zhou ◽  
S. L. Chang ◽  
M. Petrick

Abstract A comprehensive radiation heat transfer model and a reduced NOx kinetics model were coupled with a computational fluid dynamics (CFD) code and then used to investigate the radiation heat transfer, pollutant formation and flow characteristics in a glass furnace. The radiation model solves the spectral radiative transport equation in the combustion space of emitting and absorbing media, i.e., CO2, H2O, and soot and emission/reflection from the furnace crown. The advanced numerical scheme for calculating the radiation heat transfer is extremely effective in conserving energy between radiation emission and absorption. A parametric study was conducted to investigate the impact of operating conditions on the furnace performance with emphasis on the investigation into the formation of NOx.


Author(s):  
Fiaz Mahmood ◽  
Huasi Hu

Because of relaxed requirements on laser-beam uniformity and reduced sensitivity to hydrodynamic instabilities, the ICF Program has concentrated the most of its effort, on the X-ray or indirect drive approach to ICF since 1976. In indirect drive ICF, the driver energy, from laser beams or ion beams, is first absorbed in a high-Z closed cavity which surrounds the capsule, called “hohlraum”. The material heated by the driver emits X-rays, which ultimately drive the capsule implosion. For optimally designed targets, almost 70%–80% of the driver energy can be converted to X-rays. Our main focus is on the view factor calculations for hohlraum geometry of the laser driven indirect ICF approach. This analysis is very important to symmetrically irradiate the ICF capsule. View factor calculations has different radiation heat transfer applications, especially, for indirect drive ICF. In the present work, the obstructed view factor calculations for a square geometry are performed using crossed strings method. For view factor evaluation of the radiation heat transport calculations, different methods are being used. The crossed strings method is much more reliable for simple geometries among the available view factor evaluation techniques. Different cases have been studied for the view factor calculations. These cases include the view factor calculations; if radiations are emitted either from horizontal or vertical axis and a special case for the obstructed view factor calculations. When a third surface is involved in the two already existing surfaces the view factor is said to be the obstructed one rather than the unobstructed ones. Shadow effect method is used for the obstructed view factor calculations. On the other hand, obstructed view factors are computed by subtracting the view factors to the shadows of the obstruction polygons from the unobstructed view factor. The multiple overlaps could become quite complicated while calculating obstructed view factors. Two distinct computer programmes are developed and improved using FORTRAN-90 to evaluate obstructed and unobstructed view factors, for a square geometry. Radiation emission, from both horizontal and vertical surfaces, is considered for calculation of obstructed and unobstructed view factors. The programmes are liabile of calculation for the view factors of variable length of the square square geometry in both horizontal and vertical directions, respectively. In the case of obstructed view factors calculations, certain degree of error was expected. Bench mark of the developed programmes is performed using “Summation Rule”. For the error estimation the unobstructed and obstructed view factors are compared for the similar geometry and found in good agreement, showing the accuracy and reliability of the programmes.


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