CFD analysis of a scramjet combustor with cavity based flame holders. (March 2018)
- Record Type:
- Journal Article
- Title:
- CFD analysis of a scramjet combustor with cavity based flame holders. (March 2018)
- Main Title:
- CFD analysis of a scramjet combustor with cavity based flame holders
- Authors:
- Kummitha, Obula Reddy
Pandey, Krishna Murari
Gupta, Rajat - Abstract:
- Abstract: Numerical analysis of a scramjet combustor with different cavity flame holders has been carried out using ANSYS 16 - FLUENT tool. In this research article the internal fluid flow behaviour of the scramjet combustor with different cavity based flame holders have been discussed in detail. Two dimensional Reynolds-Averaged Navier-Stokes governing(RANS) equations and shear stress turbulence (SST) k − ω model along with finite rate/eddy dissipation chemistry turbulence have been considered for modelling chemical reacting flows. Due to the advantage of less computational time, global one step reaction mechanism has been used for combustion modelling of hydrogen and air. The performance of the scramjet combustor with two different cavities namely spherical and step cavity has been compared with the standard DLR scramjet. From the comparison of numerical results, it is found that the development of recirculation regions and additional shock waves from the edge of cavity flame holder is increased. And also it is observed that with the cavity flame holder the residence time of air in the scramjet combustor is also increased and achieved stabilized combustion. From this research analysis, it has been found that the mixing and combustion efficiency of scramjet combustor with step cavity design is optimum as compared to other models. Highlights: Comparison is made for a scramjet with and without cavity flame holder. The residence time is increased with the presence of cavityAbstract: Numerical analysis of a scramjet combustor with different cavity flame holders has been carried out using ANSYS 16 - FLUENT tool. In this research article the internal fluid flow behaviour of the scramjet combustor with different cavity based flame holders have been discussed in detail. Two dimensional Reynolds-Averaged Navier-Stokes governing(RANS) equations and shear stress turbulence (SST) k − ω model along with finite rate/eddy dissipation chemistry turbulence have been considered for modelling chemical reacting flows. Due to the advantage of less computational time, global one step reaction mechanism has been used for combustion modelling of hydrogen and air. The performance of the scramjet combustor with two different cavities namely spherical and step cavity has been compared with the standard DLR scramjet. From the comparison of numerical results, it is found that the development of recirculation regions and additional shock waves from the edge of cavity flame holder is increased. And also it is observed that with the cavity flame holder the residence time of air in the scramjet combustor is also increased and achieved stabilized combustion. From this research analysis, it has been found that the mixing and combustion efficiency of scramjet combustor with step cavity design is optimum as compared to other models. Highlights: Comparison is made for a scramjet with and without cavity flame holder. The residence time is increased with the presence of cavity flame holder. Step cavity design achieved optimum performance. … (more)
- Is Part Of:
- Acta astronautica. Volume 144(2018)
- Journal:
- Acta astronautica
- Issue:
- Volume 144(2018)
- Issue Display:
- Volume 144, Issue 2018 (2018)
- Year:
- 2018
- Volume:
- 144
- Issue:
- 2018
- Issue Sort Value:
- 2018-0144-2018-0000
- Page Start:
- 244
- Page End:
- 253
- Publication Date:
- 2018-03
- Subjects:
- Scramjet -- SST k−ω model -- Cavity flame holder -- Mixing efficiency -- Combustion efficiency -- Bow shock -- Recirculation zones
Astronautics -- Periodicals
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629.405 - Journal URLs:
- http://www.sciencedirect.com/science/journal/00945765 ↗
http://www.elsevier.com/journals ↗ - DOI:
- 10.1016/j.actaastro.2018.01.005 ↗
- Languages:
- English
- ISSNs:
- 0094-5765
- Deposit Type:
- Legaldeposit
- View Content:
- Available online (eLD content is only available in our Reading Rooms) ↗
- Physical Locations:
- British Library DSC - 0596.750000
British Library DSC - BLDSS-3PM
British Library HMNTS - ELD Digital store - Ingest File:
- 11341.xml