• Bhavik n solanki
• Dr. Umang J. Patdiwala

Analysis of Effect of flow over NACA 6409 aerofoil linear cascade was done using the available Computational Fluid Dynamics methods. Popular CAE software ANSYS CFX was used for analyzation and simulation. The coordinates were imported to the geometry modeller of ANSYS. CFX (Fluid Flow) was used to generate mesh and conduct the experimentation. At the end of modelling and meshing, simulation was done to observe the effect of flow at a high Reynolds number, on the said aerofoil model with respect to pressure distribution and various aerodynamic forces while maintaining variation in its angle of attack.

Aerofoil, Linear cascade, Wind Tunnel, Computational Fluid Dynamics, ANSYS

"Simulation of Aerofoil for Linear Cascade ", International Journal of Emerging Technologies and Innovative Research (www.jetir.org), ISSN:2349-5162, Vol.6, Issue 6, page no.212-215, June 2019, Available :http://www.jetir.org/papers/JETIR1907U61.pdf

"Simulation of Aerofoil for Linear Cascade ", International Journal of Emerging Technologies and Innovative Research (www.jetir.org | UGC and issn Approved), ISSN:2349-5162, Vol.6, Issue 6, page no. pp212-215, June 2019, Available at : http://www.jetir.org/papers/JETIR1907U61.pdf