Zobrazeno 1 - 10
of 14
pro vyhledávání: '"Mukkarum Hussain"'
Autor:
Mukkarum Hussain, Iftikhar Ahmed, Ilyas Khan, Chu Anh My, Mirza Mehmood Baig, Afrasyab Khan, Stanislav S. Makhanov
Publikováno v:
Case Studies in Thermal Engineering, Vol 26, Iss , Pp 101025- (2021)
A successful ignition is the consequence of corresponding conditions of fuel mass flow rates, mixture ratio, as well as initiation energy in time and space. If ignition does not take place accurately, serious damages can take place within or outside
Externí odkaz:
https://doaj.org/article/7b540ecbdf584cc0856cb43ba4261764
Publikováno v:
Energies, Vol 15, Iss 16, p 6079 (2022)
Solid fuel combustion in a chamber does not necessarily occur at a constant rate and may show fluctuations due to variables such as varying burning rates, chamber pressure, and residual combustion. These variables can cause the fuel to burn dispropor
Externí odkaz:
https://doaj.org/article/6606a8fb2b6a46af83192b458d631e8e
Publikováno v:
Results in Physics, Vol 7, Iss , Pp 1261-1273 (2017)
Precise aerodynamics performance prediction plays key role for a flying vehicle to get its mission completed within desired accuracy. Aerodynamic coefficients for same Mach number can be different at different altitude due to difference in Reynolds n
Externí odkaz:
https://doaj.org/article/a412b389e89b40c3815d55178fc3bb00
Publikováno v:
Journal of Applied Fluid Mechanics, Vol 9, Iss 4, Pp 2073-2081 (2016)
Total Variation Diminishing (TVD) schemes are low dissipative and high resolution schemes but bounded by stability criterion CFL
Externí odkaz:
https://doaj.org/article/d977a020e30d4014ab5d47452b43d118
Publikováno v:
2022 19th International Bhurban Conference on Applied Sciences and Technology (IBCAST).
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::78e82acba91acf11a3ab897c148b442e
https://doi.org/10.1109/ibcast54850.2022.9990249
https://doi.org/10.1109/ibcast54850.2022.9990249
Autor:
Mukkarum Hussain, Noor Fatima Siddiqui
Publikováno v:
Journal of Mechanical Science and Technology. 34:1185-1193
The resolution of Harten’s non-oscillatory explicit second-order accurate total variation diminishing scheme was relatively high for computations of nonlinear wave equations. However, this scheme shows false dissipation for sharp discontinuities, s
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::df92323b07282f2aa21b144194e65100
https://doi.org/10.1007/s12206-020-0219-z
https://doi.org/10.1007/s12206-020-0219-z
Publikováno v:
Arabian Journal for Science and Engineering. 44:5889-5895
Combustion of cryogenic propellants is of great technological interest for researchers and scientists nowadays. Due to high specific impulse, the use of liquid oxygen and hydrogen as cryogenic propellants will have preferences in the years to come. I
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::cc7259de36556c4b84d9f48fc9fff606
https://doi.org/10.1007/s13369-019-03774-1
https://doi.org/10.1007/s13369-019-03774-1
Autor:
Afrasyab Khan, Mukkarum Hussain, Iftikhar Ahmed, Mirza Mehmood Baig, Chu Anh My, Ilyas Khan, Stanislav S. Makhanov
Publikováno v:
Case Studies in Thermal Engineering, Vol 26, Iss, Pp 101025-(2021)
A successful ignition is the consequence of corresponding conditions of fuel mass flow rates, mixture ratio, as well as initiation energy in time and space. If ignition does not take place accurately, serious damages can take place within or outside
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::86f6c8c34d1e0dd2ce6f45c1ed693b8f
https://doi.org/10.1016/j.csite.2021.101025
https://doi.org/10.1016/j.csite.2021.101025
Publikováno v:
Arabian Journal for Science and Engineering. 43:3807-3813
Explicit formulation of one-dimensional Euler equation with TVD scheme is bounded by the stability criterion $$\hbox {CFL}
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::968efbdff3418320fc2606e8408268ad
https://doi.org/10.1007/s13369-017-2876-5
https://doi.org/10.1007/s13369-017-2876-5
Publikováno v:
Results in Physics, Vol 7, Iss, Pp 1261-1273 (2017)
Precise aerodynamics performance prediction plays key role for a flying vehicle to get its mission completed within desired accuracy. Aerodynamic coefficients for same Mach number can be different at different altitude due to difference in Reynolds n
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::0e0a2fe08d42bfadcacb25a83c45c517
https://doi.org/10.1016/j.rinp.2017.03.020
https://doi.org/10.1016/j.rinp.2017.03.020