タイトル | Numerical modeling for primary atomization of liquid jets |
著者(英) | Przekwas, A. J.; Chuech, S. G.; Singhal, A. K. |
著者所属(英) | Computational Fluid Dynamics Research Corp. |
発行日 | 1989-01-01 |
言語 | eng |
内容記述 | In the proposed numerical model for primary atomization, surface-wave dispersion equations are solved in conjunction with the jet-embedding technique of solving mean flow equations of a liquid jet. Linear and approximate nonlinear models have been considered. In each case, the dispersion equation is solved over the whole wavelength spectrum to predict drop sizes, frequency, and liquid-mass breakup rates without using any empirical constants. The present model has been applied to several low-speed and high-speed jets. For the high-speed case (the LOX/H2 coaxial injector of the Space Shuttle Main Engine Preburner), predicted drop sizes and liquid breakup rates are in good agreement with the results of the CICM code, which have been calibrated against measured data. |
NASA分類 | FLUID MECHANICS AND HEAT TRANSFER |
レポートNO | 89A25145 AIAA PAPER 89-0163 |
権利 | Copyright |
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