A copy of this work was available on the public web and has been preserved in the Wayback Machine. The capture dates from 2015; you can also visit the original URL.
The file type is
A B S T R A C T Compressible gas flow inside a convergent-divergent nozzle and its exhaust plume at different nozzle pressure ratios (NPR) have been numerically studied with several turbulence models. The numerical results reveal that, the SST k-ω model give the best results compared with other models in time and accuracy. The effect of changes in value of divergence half-angle ( ) on the nozzle performance, thrust coefficient ( f C ) and discharge coefficient ( d C ) has been investigatedfatcat:xxsv3e27ijc7vmt5rv5qmvjzqe