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  1. 1
    CFD-based optimization of base pressure behavior on suddenly expanded flows at supersonic Mach numbers

    CFD-based optimization of base pressure behavior on suddenly expanded flows at supersonic Mach numbers by Jaimon, Dennis Quadros, Khan, Sher Afghan, Prashanth, T.

    Published 2022
    “…: The base pressure developed in a suddenly expanded flow process majorly depends on Mach number (M), nozzle pressure ratio (NPR), area ratio (AR), and length to diameter ratio (L/D). …”
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  2. 2
    Prediction of base pressure in a suddenly expanded flow the processes at supersonic Mach Number Regimes using ANN and CFD

    Prediction of base pressure in a suddenly expanded flow the processes at supersonic Mach Number Regimes using ANN and CFD by Quadros, Jaimon Dennis, Khan, Sher Afghan

    Published 2020
    “…This was done by the design of experiments based L27 Orthogonal array. The three input parameters were Mach number (M), nozzle pressure ratio (NPR) and area ratio (AR) and base pressure was the output parameter. …”
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  3. 3
    Prediction of base pressure in a suddenly expanded flow process at supersonic mach number regimes using ANN and CFD

    Prediction of base pressure in a suddenly expanded flow process at supersonic mach number regimes using ANN and CFD by Quadros, Jaimon Dennis, Khan, Sher Afghan

    Published 2020
    “…This was done by the design of experiments based L27 Orthogonal array. The three input parameters were Mach number (M), nozzle pressure ratio (NPR) and area ratio (AR) and base pressure was the output parameter. …”
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  4. 4
    Modeling and validation of base pressure for aerodynamic vehicles based on machine learning models

    Modeling and validation of base pressure for aerodynamic vehicles based on machine learning models by Quadros, Jaimon Dennis, Khan, Sher Afghan, Aabid, Abdul, Baig, Muneer

    Published 2023
    “…Based on the identical dataset, the GA-BP and PSO-BP algorithms are also compared to the PCA-BAS-ENN algorithm. …”
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  5. 5
    Base drag estimation in suddenly expanded supersonic flows using backpropagation genetic and recurrent neural networks

    Base drag estimation in suddenly expanded supersonic flows using backpropagation genetic and recurrent neural networks by Jaimon, Dennis Quadros, Prashanth, T., Khan, Sher Afghan

    Published 2022
    “…The objective of forwarding mapping (FM) is to predict the responses, namely base pressure (β), base pressure with the cavity (βcav), and base pressure with rib (βrib), for a known combination of flow and geometric parameters, namely Mach number (M), nozzle pressure ratio (η), area ratio (α), and length to diameter ratio (ψ). …”
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  6. 6
    Solution of Navier-Stokes equations by fourth-order compact schemes and AUSM flux splitting

    Solution of Navier-Stokes equations by fourth-order compact schemes and AUSM flux splitting by Mawlood M.K., Basri S., Asrar W., Omar A.A., Mokhtar A.S., Ahmad M.M.H.M.

    Published 2023
    “…Design/methodology/approach - A numerical algorithm based on high-order compact finite-difference schemes is developed for solving Navier-Stokes equations in two-dimensional space. …”
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  7. 7
    Solution of Navier-Stokes equations by fourth-order compact schemes and AUSM flux splitting

    Solution of Navier-Stokes equations by fourth-order compact schemes and AUSM flux splitting by Mawlood, M.K., Basri, S., Asrar, Waqar, Omar, Ashraf Ali, Mokhtar, A.S., Ahmad, M.M.

    Published 2006
    “…Design/methodology/approach – A numerical algorithm based on high-order compact finite-difference schemes is developed for solving Navier-Stokes equations in two-dimensional space. …”
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  8. 8
    New tunable all-fiber optical comb filter based on machzehnder interferometer

    New tunable all-fiber optical comb filter based on machzehnder interferometer by Islam, Md. Shafiqul

    Published 2011
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