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airfoil modeling
Posted 2010年7月11日 GMT-4 10:43 1 Reply
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Hi
I am trying to modeling the flow separation from the airfoil (NACA0015) by Comsol 3.5a. after I click on the solve bottom show the error as below:
Error: 6170
Failed to evaluate variable.
- Variable: T
- Geometry: 1
- Subdomain: 1
Failed to evaluate variable.
- Variable: rho_ns
- Defined as: ((unit_kg_cf*mat1_rho((T/unit_K_cf)))/(unit_m_cf^3))
Failed to evaluate expression.
- Expression: nojac(rho_ns)
Failed to evaluate expression.
- Expression: d((((nojac(rho_ns)*((nojac(u)*vx)+(nojac(v)*vy)))+py)-(nojac(eta_ns)*((vxx+uyx)+(vyy*2)))),vy)
I attach the comsol file by this message.
If would possible to everyone to help me to solve this problem.
hasan
I am trying to modeling the flow separation from the airfoil (NACA0015) by Comsol 3.5a. after I click on the solve bottom show the error as below:
Error: 6170
Failed to evaluate variable.
- Variable: T
- Geometry: 1
- Subdomain: 1
Failed to evaluate variable.
- Variable: rho_ns
- Defined as: ((unit_kg_cf*mat1_rho((T/unit_K_cf)))/(unit_m_cf^3))
Failed to evaluate expression.
- Expression: nojac(rho_ns)
Failed to evaluate expression.
- Expression: d((((nojac(rho_ns)*((nojac(u)*vx)+(nojac(v)*vy)))+py)-(nojac(eta_ns)*((vxx+uyx)+(vyy*2)))),vy)
I attach the comsol file by this message.
If would possible to everyone to help me to solve this problem.
hasan
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1 Reply Last Post 2010年7月11日 GMT-4 14:36