ANSYS FLUENT AIRFOIL
ANSYS FLUENT AIRFOIL Good afternoon at all. Follow below flow around an airfoil simulation. Was made comparative study for two situations. First: attack angle is 5�, stability condition. Second: attack angle is 25�, above critical angle, creating instability condition fly, called stall. The Mach number is 0.9 for the two cases. The simulation was made in Ansys Fluent. Boa tarde a todos. Segue abaixo simula��o do fluxo de ar em torno de um aerof�lio. Foi realizado estudo comparativo para duas situa��es. Primeira: �ngulo de ataque igual a 5 graus, condi��o de estabilidade. Segunda: �ngulo de ataque igual a 25 graus, gerando instabilidade na condi��o de voo, conhecida como estol. A simula��o foi realizada no Ansys Fluent. Attack angle - 5� (stability condition) Attack angle - 25� (stall) ANGLE ATTACK - 5� Velocity Pressure Temperature ANGLE ATTACK - 25� Pressure Temperature Velocity visit link download
