Numerical study of non-reacting flowfields of a swirling trapped vortex ramjet combustor

2018 ◽  
Vol 74 ◽  
pp. 81-92 ◽  
Author(s):  
Song Chen ◽  
Dan Zhao
Keyword(s):  
Numerical Study ◽  
Ramjet Combustor ◽  
Trapped Vortex

Numerical Investigation of a Trapped Vortex Miniature Ramjet Combustor

2015 ◽  
Vol 31 (3) ◽  
pp. 872-882 ◽  
Author(s):  
Song Chen ◽  
Randy S. M. Chue ◽  
Jörg Schlüter ◽  
Tue T. Q. Nguyen ◽  
Simon C. M. Yu
Keyword(s):  
Numerical Investigation ◽  
Ramjet Combustor ◽  
Trapped Vortex

scholarly journals Numerical study of flame/vortex interactions in 2-D Trapped Vortex Combustor

2014 ◽  
Vol 18 (4) ◽  
pp. 1373-1387 ◽  
Author(s):  
Prasad Mishra ◽  
Renganathan Sudharshan ◽  
Kumar Ezhil
Keyword(s):  
Numerical Study ◽  
Flame Structure ◽  
Reaction Rates ◽  
Operating Conditions ◽  
Navier Stokes ◽  
Base Case ◽  
Primary Vortex ◽  
Vortex Interactions ◽  
Wide Range ◽  
Trapped Vortex

The interactions between flame and vortex in a 2-D Trapped Vortex Combustor are investigated by simulating the Reynolds Averaged Navier Stokes (RANS) equations, for the following five cases namely (i) non-reacting (base) case, (ii) post-vortex ignition without premixing, (iii) post-vortex ignition with premixing, (iv) pre-vortex ignition without premixing and (v) pre-vortex ignition with premixing. For the post-vortex ignition without premixing case, the reactants are mixed well in the cavity resulting in a stable ?C? shaped flame along the vortex edge. Further, there is insignificant change in the vorticity due to chemical reactions. In contrast, for the pre-vortex ignition case (no premixing); the flame gets stabilized at the interface of two counter rotating vortices resulting in reduced reaction rates. There is a noticeable change in the location and size of the primary vortex as compared to case (ii). When the mainstream air is premixed with fuel, there is a further reduction in the reaction rates and thus structure of cavity flame gets altered significantly for case (v). Pilot flame established for cases (ii) and (iii) are well shielded from main flow and hence the flame structure and reaction rates do not change appreciably. Hence, it is expected that cases (ii) and (iii) can perform well over a wide range of operating conditions.

scholarly journals Numerical study on a new design of solid-fuel ramjet combustor with swirl flow

2019 ◽  
Vol 8 (2) ◽  
pp. 72-79
Author(s):  
Omer Musa ◽  
Chen Xiong ◽  
Guoping Huang
Keyword(s):  
Heat Transfer ◽  
Parallel Computing ◽  
Fluid Mechanics ◽  
Chemical Kinetics ◽  
Solid Fuel ◽  
Numerical Study ◽  
Swirl Flow ◽  
Ramjet Combustor ◽  
Afterburning Chamber ◽  
Transfer Thermodynamics

A new design of solid-fuel ramjet is proposed and examined numerically in this paper. Multi-physics coupling code is developed using FORTRAN and parallel computing to solve the problems of multi-physics coupling of fluid mechanics, solid pyrolysis, heat transfer, thermodynamics, and chemical kinetics. Simulations are carried out for the proposed design then the results are compared with the classic design of the solid-fuel ramjet. It is found that the proposed design has improved the regression rate significantly; besides, the amount of released solid fuel is increased for the same size. A new flame has been observed inside the combustion chamber of the proposed design then the two flamed were emerged in the afterburning chamber.

Numerical study of the low-frequency atomic dynamics in a Lennard-Jones glass

1998 ◽  
Vol 77 (2) ◽  
pp. 473-484 ◽  
Author(s):  
M. Sampoli, P. Benassi, R. Dell'Anna,
Keyword(s):  
Numerical Study ◽  
Low Frequency ◽  
Lennard Jones
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