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�
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ANGLE ATTACK - 25�
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