nozzle efficiencyPrandtl-Meyer theoryturbine nozzleMach number and the speed of sound Isentropic flow with area change Normal shocks Influence of friction in flow through straight nozzles Supersaturation Prandtl–Meyer expansion Flow leaving a turbine nozzle...
Gas flows through nozzles and diffusers show an interesting behavior when their speed reaches, or is above, the speed of sound of the gas. This behavior must be well understood for the proper design of devices and engines. In this section we study the laws that govern the transition from ...
Compressible Flow in a Nozzle 青云英语翻译 请在下面的文本框内输入文字,然后点击开始翻译按钮进行翻译,如果您看不到结果,请重新翻译! 翻译结果1翻译结果2翻译结果3翻译结果4翻译结果5 翻译结果1复制译文编辑译文朗读译文返回顶部 可压缩流在喷嘴 翻译结果2复制译文编辑译文朗读译文返回顶部...
In this chapter we study the laws that govern the transition from sub-to supersonic flow and vice-versa, and draw relevant conclusions for the design of nozzles and diffusers, and for rocket motors. We will see that subsonic nozzles have a converging cross section, while supersonic nozzles...
Discharge Coefficients for Compressible Flow Through Small-Diameter Orifices and Convergent Nozzles - Kayser, Shambaugh - 1991Kayser, J. C. and Shambaugh, R. L., "Discharge Coefficients for Compressible Flow Through Small-Diameter Orifices and Convergent Nozzles," Chemical Engineering Science, Vol. ...
Computational study of the gas flow through a critical nozzle The critical nozzle is defined as a device to measure the mass flow with only the nozzle supply conditions making use of the flow choking phenomenon at the... H-D,Kim,J-H,... - 《Proceedings of the Institution of Mechanical ...
This will first occur at the throat, d, and henceforth, the flow field upstream of the throat will remain frozen as sound waves with the information about conditions in b cannot travel through the throat against the flow. From then on, mass flow through the nozzle remains constant and the ...
Simulation and validation of compressible flow in nozzle geometries and validation of OpenFOAM for this application. Institute of Fluid Dynamics, ETH Zurich, 2007. (PhD Thesis).B. W thrich, "Simulation and Validation of Compressible Flow in Nozzle Geometries and Validation of OpenFOAM f...
We present results from high-order accurate large-eddy simulations of compressible flow through convergent-divergent nozzles with and without bell-shaped divergent portions. The nozzles have isothermal walls and circular cross-sections. The incoming flow is a turbulent, subsonic fully-developed pipe flo...
hi im trying to model compressible fluid flow, from nozzle exhaust. i want to calculate temperature distribution of the exhaust plume at some depth. the exhaust plume is going to the deflector, so the temperature distribution at a point on deflector is to be calculated.i want to first model...