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Manoj T. Nair

Indian Institute of Technology Kanpur

15

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162

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Three-level order-adaptive weighted essentially non-oscillatory schemes

2021
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Numerical study of shock -boundary layer interaction in hypersonic flow

2007
- K. Kumar
- Manoj T. Nair
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Computational Analysis of Inlet Aerodynamics for a Hypersonic Research Vehicle

2005 Journal of Propulsion and Power
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Reynolds Averaged Navier-Stokes Based Aerodynamic Analysis of Inlet for a Hypersonic Research Vehicle AIAA-2003-7067

2003
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UPWIND SCHEMES AND LARGE EDDY SIMULATION

1999 International Journal for Numerical Methods in Fluids
- Tapan K. Sengupta
- Manoj T. Nair
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FLOW PAST ROTATING CYLINDERS AT HIGH REYNOLDS NUMBERS USING HIGHER ORDER UPWIND SCHEME

1998 Computers & Fluids
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Onset of asymmetry : Flow past circular and elliptic cylinders

1996 International Journal for Numerical Methods in Fluids
- Manoj T. Nair
- Tapan K. Sengupta
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