Simulations of cloud condensation droplet nucleation and growth

1989 ◽  
Author(s):  
L. L. Edwards
2018 ◽  
Vol 140 (10) ◽  
Author(s):  
V. Babu

A simple procedure for calculating the pressure at the onset and termination of condensation shocks that occur in steam nozzles and steam turbine blade passages is presented. In addition, the location of the termination of the condensation shock with reference to the throat location is also predicted. The procedure is based entirely on thermodynamic and gas dynamic considerations, without using a model for droplet nucleation and growth and the nozzle profile. The only input required is the stagnation condition at the inlet to the nozzle. The procedure requires the solution of a system of algebraic equations which can be accomplished quite easily. Calculations have been carried out for several inlet stagnation conditions and the predictions are compared with the available experimental data. The agreement is seen to be reasonable considering the simplicity of the procedure.


Author(s):  
F Bakhtar ◽  
A J White ◽  
H Mashmoushy

During the course of expansion of steam in turbines, the state path crosses the saturation line and hence subsequent turbine stages operate with wet steam. These stages have lower thermodynamic efficiencies than those operating in the superheated region, and currently the phenomena contributing to the increased losses are not fully understood. The development of the nucleation theory has opened the way for the study of condensing flows in turbines. As, with the advances in numerical methods, the equations describing droplet nucleation and growth rates can be combined with the field conservation equations and the set treated numerically, which allows the behaviour of complex nucleating and wet steam flows in turbines to be analysed. This paper outlines and reviews wet steam calculation methods and discusses comparisons between numerical and experimental results. For the most part, the comparisons presented are based on work of the authors and their co-workers, but some more recent calculations by other investigators are also included.


1999 ◽  
Vol 50 (3-4) ◽  
pp. 289-315 ◽  
Author(s):  
Bengt G Martinsson ◽  
Göran Frank ◽  
Sven-Inge Cederfelt ◽  
Erik Swietlicki ◽  
Olle H Berg ◽  
...  

2008 ◽  
Vol 129 (23) ◽  
pp. 234507 ◽  
Author(s):  
Mark J. Uline ◽  
David S. Corti

2017 ◽  
Vol 167 ◽  
pp. 204-218 ◽  
Author(s):  
G. Neuber ◽  
A. Kronenburg ◽  
O.T. Stein ◽  
M.J. Cleary

Langmuir ◽  
2020 ◽  
Vol 36 (45) ◽  
pp. 13716-13724
Author(s):  
Guihua Tang ◽  
Dong Niu ◽  
Lin Guo ◽  
Jinliang Xu

Author(s):  
Ashish Alex Sam ◽  
Keerthi Raj Kunniyoor ◽  
Jayachandran K. Narayanan ◽  
Arpit Mishra ◽  
Parthasarathi Ghosh

Cryogenic turboexpanders for nitrogen refrigeration and liquefaction cycles operating near liquefaction conditions are vulnerable to droplet formation. The turboexpander must be devoid of any traces of droplets, as this may cause damage to the blades and also result in performance deterioration. Hence, a multiphase flow analysis was conducted, based on the droplet condensation model in Ansys CFX®, to identify any possible droplet sites and its nature of propagation. A single-phase steady state simulation of the turboexpander was performed initially to identify the regions susceptible to droplet formation, followed by a multiphase analysis to study the flow field behavior and to characterize the droplet nucleation and growth. It has been observed that the low-pressure regions like vortices and wakes are susceptible to sub-cooling and thereby in droplet formation. Also, major geometrical parameters that affect the droplet nucleation have also been identified.


Author(s):  
F Bakhtar ◽  
R Mohsin

In the course of expansion in turbines, steam first supercools and then nucleates to become a two-phase mixture. The fluid then consists of a very large number of extremely small droplets which are carried by and interact with the parent vapour. The formation and subsequent behaviour of the liquid phase cause problems which lower the performance of the wet stages of steam turbines. To treat such flows the general conservation equations governing the whole field are combined with those describing droplet nucleation and growth and the set treated numerically. The article examines the solution of throughflows of nucleating steam in a turbine stage using a time-marching technique. The treatment which is the refinement of an earlier one has been applied to the flow in a turbine stage. Comparisons are presented between the results of theoretical solutions and direct measurements upstream and downstream of the nucleating stage and the agreement obtained is good.


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