Numerical Simulation of Shock Induced Turbulence in a Nozzle Flow

2013 ◽  
Vol 94 (3) ◽  
pp. 229-237 ◽  
Author(s):  
M. A. Jinnah
2015 ◽  
Vol 656 ◽  
pp. 012100 ◽  
Author(s):  
Kaushik Saha ◽  
Sibendu Som ◽  
Michele Battistoni ◽  
Yanheng Li ◽  
Shaoping Quan ◽  
...  

2011 ◽  
Vol 2011.24 (0) ◽  
pp. 513-514
Author(s):  
Tsubasa OHSHIMA ◽  
Hirotoshi YANAGI ◽  
Yasuhide OKAZAKI ◽  
Koji MORINISHI

2003 ◽  
Vol 125 (6) ◽  
pp. 963-969 ◽  
Author(s):  
Weixing Yuan ◽  
Gu¨nter H. Schnerr

The present investigation demonstrates the strong interaction of cavitating nozzle flow with the outside jet formation. Due to the strong sensitivity of cavitation on the imposed boundary conditions, simulations with restriction on the internal problem are qualitatively and quantitatively incorrect, so that phenomena like hydraulic flip and supercavitation cannot be revealed. Our results indicate the potential of cavitation for enhancement of atomization and spray quality.


2020 ◽  
Vol 19 (1) ◽  
pp. 27-33
Author(s):  
L.V. Gileva ◽  
◽  
A.A. Aksenov ◽  
Yu.V. Kozhukhov ◽  
A.Yu. Petrov ◽  
...  

2018 ◽  
Vol 7 (3.29) ◽  
pp. 243
Author(s):  
Sher Afghan Khan ◽  
Mir Owais Ali ◽  
Miah Mohammed Riyadh ◽  
Zahid Hossen ◽  
Nafis Mahdi Arefin

A numerical simulation was carried out to compare various turbulence models simulating axisymmetric nozzle flow past suddenly expanded ducts. The simulations were done for L/D = 10. The convergent-divergent nozzle has been modeled and simulated using the turbulence models: The Standard k-ε model, The Standard k-ω model and The SST k-ω model. Numerical simulations were done for Mach numbers 1.87, 2.2, and 2.58 and the nozzles were operated for NPRs in the range from 3 to 11. From the numerical analysis it is apparent that for a given Mach number and effect of NPR will result in maximum gain or loss of pressure. Numerical results are in good agreement with the experimental results.  


2017 ◽  
Author(s):  
Pedro Marti-Aldaravi ◽  
Kaushik Saha ◽  
Jaime Gimeno ◽  
Sibendu Som

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