Flow Behaviour on Elbow With Various
      Geometries of Nozzle

The aerofoils which allow for the flow at a broader range of angles have a more significant impact on the power generation from the turbine. The conception and examination for the aerofoil geometry have been executed in the current work to evaluate the behaviour of the flow in terms of the velocity and pressure lineation. The work is intended to focus on analysing the flow behaviour along the surface of the aerofoil geometry. The aerofoil geometries are opted to be of new aerofoil type of NACA 8412 series. The aerofoil geometry was analysed for a constant angle of attack along the total length. This evaluation was done for the angle of attack ranging from 0° to 20° with 5° interval for each model. The inlet velocity for the flow along the surface of the aerofoil geometry was taken varied from 7.5 m/s to 10 m/s with 0.5 m/s interval for each model. The plot points for the geometries are generated using the Auto CAD for different angles. The further simulations and evaluations were executed using the Ansys Fluent software. On evaluating and considering the variable conditions, the optimum values are obtained for the aerofoil at 15° angle of inclination at an inlet velocity of 9 m/s. The software generated results when compared to the regression data generated ascertained to be in a good correlation with each other.

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Comparative Study on Stepped Heat Pipe Using CFD

AKHIL¹,

Sashank²,

Nikhil³

et al. 2020

JME

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Flow Behaviour on Elbow With Various Geometries of Nozzle

Cited by 4 publications

References 10 publications

Comparative study of different pipe geometries using CFD

Comparative study of different pipe geometries using CFD

Flow behaviour on aerofoils using CFD

Comparative Study on Stepped Heat Pipe Using CFD

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