Numerical simulation of supersonic and turbulent combustion with trans-verse sonic fuel injection
Complicated interacting flow features such as shock-wave, boundary-layer and shock induced combustion are simulated numerically in the current study to investigate the effect of the transverse sonic fuel injection on the air-fuel mixing and flame stabilisation. The flow is modelled using the Reyn...
| Main Authors: | , , , |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
Inderscience Publishers
2015
|
| Subjects: | |
| Online Access: | http://irep.iium.edu.my/43827/ http://irep.iium.edu.my/43827/ http://irep.iium.edu.my/43827/ http://irep.iium.edu.my/43827/1/2015-Numerical_simulation_of_supersonic_and_turbulent_combustion_with_transverse_sonic_fuel_injection-IJESMS.pdf |
| id |
iium-43827 |
|---|---|
| recordtype |
eprints |
| spelling |
iium-438272015-07-21T05:20:57Z http://irep.iium.edu.my/43827/ Numerical simulation of supersonic and turbulent combustion with trans-verse sonic fuel injection Kamel, Mohammed Owis, Farouk Idres, Moumen Hashem, Aly TJ Mechanical engineering and machinery Complicated interacting flow features such as shock-wave, boundary-layer and shock induced combustion are simulated numerically in the current study to investigate the effect of the transverse sonic fuel injection on the air-fuel mixing and flame stabilisation. The flow is modelled using the Reynolds-averaged Navier-stocks (RANS) equations, where chemical kinetics model is employed to compute the finite rates of chemical reactions. Turbulence is modelled using the Baldwin-Lomax algebraic model. Finite-volume scheme is applied where the convective fluxes are discretised by second order accurate Roe’s scheme using MUSCL approach. Second order accurate Runge-Kutta method is used for the time-integration. Turbulent and chemically-reacting supersonic flow of hydrogen-air mixture over a ramp is simulated and the results show good agreement with the experimental data and the published numerical simulations In addition, air-hydrogen flow is studied in a single strut scramjet engine, where mixing and flame holding processes are carried out using fuel transverse sonic injection. Inderscience Publishers 2015 Article PeerReviewed application/pdf en http://irep.iium.edu.my/43827/1/2015-Numerical_simulation_of_supersonic_and_turbulent_combustion_with_transverse_sonic_fuel_injection-IJESMS.pdf Kamel, Mohammed and Owis, Farouk and Idres, Moumen and Hashem, Aly (2015) Numerical simulation of supersonic and turbulent combustion with trans-verse sonic fuel injection. International Journal of Engineering Systems Modelling and Simulation, 7 (2). pp. 35-61. ISSN 1755-9766 http://www.inderscience.com/ 10.1504/IJESMS.2015.066132 |
| repository_type |
Digital Repository |
| institution_category |
Local University |
| institution |
International Islamic University Malaysia |
| building |
IIUM Repository |
| collection |
Online Access |
| language |
English |
| topic |
TJ Mechanical engineering and machinery |
| spellingShingle |
TJ Mechanical engineering and machinery Kamel, Mohammed Owis, Farouk Idres, Moumen Hashem, Aly Numerical simulation of supersonic and turbulent combustion with trans-verse sonic fuel injection |
| description |
Complicated interacting flow features such as shock-wave, boundary-layer and shock
induced combustion are simulated numerically in the current study to investigate the effect of the
transverse sonic fuel injection on the air-fuel mixing and flame stabilisation. The flow is
modelled using the Reynolds-averaged Navier-stocks (RANS) equations, where chemical
kinetics model is employed to compute the finite rates of chemical reactions. Turbulence is
modelled using the Baldwin-Lomax algebraic model. Finite-volume scheme is applied where the
convective fluxes are discretised by second order accurate Roe’s scheme using MUSCL
approach. Second order accurate Runge-Kutta method is used for the time-integration. Turbulent
and chemically-reacting supersonic flow of hydrogen-air mixture over a ramp is simulated and
the results show good agreement with the experimental data and the published numerical
simulations In addition, air-hydrogen flow is studied in a single strut scramjet engine, where
mixing and flame holding processes are carried out using fuel transverse sonic injection. |
| format |
Article |
| author |
Kamel, Mohammed Owis, Farouk Idres, Moumen Hashem, Aly |
| author_facet |
Kamel, Mohammed Owis, Farouk Idres, Moumen Hashem, Aly |
| author_sort |
Kamel, Mohammed |
| title |
Numerical simulation of supersonic and turbulent combustion with trans-verse sonic fuel injection |
| title_short |
Numerical simulation of supersonic and turbulent combustion with trans-verse sonic fuel injection |
| title_full |
Numerical simulation of supersonic and turbulent combustion with trans-verse sonic fuel injection |
| title_fullStr |
Numerical simulation of supersonic and turbulent combustion with trans-verse sonic fuel injection |
| title_full_unstemmed |
Numerical simulation of supersonic and turbulent combustion with trans-verse sonic fuel injection |
| title_sort |
numerical simulation of supersonic and turbulent combustion with trans-verse sonic fuel injection |
| publisher |
Inderscience Publishers |
| publishDate |
2015 |
| url |
http://irep.iium.edu.my/43827/ http://irep.iium.edu.my/43827/ http://irep.iium.edu.my/43827/ http://irep.iium.edu.my/43827/1/2015-Numerical_simulation_of_supersonic_and_turbulent_combustion_with_transverse_sonic_fuel_injection-IJESMS.pdf |
| first_indexed |
2023-09-18T21:02:23Z |
| last_indexed |
2023-09-18T21:02:23Z |
| _version_ |
1777410710102343680 |