• U. Vijaya Kumar
• Prof. Anil Kumar Rao

The investigation have been performed by using the use of the Finite volume technique. Drag forces and wall shear stresses, has been analyzed by way of ANSYS 15.Zero. A simplified and idealized finite volume model through using symmetry assumption and a non-simplified finite quantity model of method had been used in the analyses. The principal study changed into carried out on wind turbine blade of airfoil formed by way of the usage of exclusive angle of attack and inlet pressure. The evaluation outcomes show that variable degree of attitude of assault and 12 bar of inlet strain offers absolute convergence on strain and drag forces in addition to wall fluxes, Validation and optimization is completed to determine the impact of drag forces, velocity, and strain distribution of various inlet strain operating situation. The natural frequency is analyzed in blade of axial waft, thus 3rd mode of herbal frequency shows top-rated convergence at 30degree

natural frequency, Airfoil.

"Validation of Wind Turbine Blade for Optimization in Pressure distribution on upper surface of Airfoil to Enhance the Performance during different inlet Pressure by using Finite Volume Method", International Journal of Emerging Technologies and Innovative Research (www.jetir.org), ISSN:2349-5162, Vol.5, Issue 6, page no.345-353, June-2018, Available :http://www.jetir.org/papers/JETIR1806438.pdf

"Validation of Wind Turbine Blade for Optimization in Pressure distribution on upper surface of Airfoil to Enhance the Performance during different inlet Pressure by using Finite Volume Method", International Journal of Emerging Technologies and Innovative Research (www.jetir.org | UGC and issn Approved), ISSN:2349-5162, Vol.5, Issue 6, page no. pp345-353, June-2018, Available at : http://www.jetir.org/papers/JETIR1806438.pdf