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  1. 1
    Mathematical Model of Boundary Layer Flow over a Moving Plate in a Nanofluid with Viscous Dissipation
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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
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  3. 3
    Study of effect of flow parameters on base pressure in a suddenly expanded duct at supersonic mach number regimes using CFD and design of experiments
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