- #1
SimoneC618
- 1
- 1
- Homework Statement
- Analyze the flux properties in an ICE manifold using 1D numerical methods such as Lax-Wendroff or Lax-Friederichs
- Relevant Equations
- initial conditions: P_0 = 101325 Pa; T_0 = 293,15 K.
Hi everyone,
i'm very new to the forum so i hope I've used the correct form to write my question.
Anyway, i need some help to evaluate the result of my last analysis: I'm studying the flux flowing inside an ICE aspiration manifold in a very simplified way (1D flux, ideal gas, compressible flow). For the analysis I've implemented the Matlab code for a Lax-Wendroff scheme and for a Lax-Friderichs scheme using the following assumptions:
the air aspirated in the manifold is initially in the ambient condition;
the conditions at the inlet could be find using the energy and mass conservation law that give: T1 = 293.08 K ; P1 = 95421.5 Pa ; u1 = 2.77 m/s.
the pressure value at the outlet can be found assuming the rotation speed of the engine (n = 6000 rpm) and knowing the geometry of the cylinder;
the value I've found is about 5kPa, so P2 = 90161 Pa
Now, i have to solve the mass, momentum and energy conservation in the conservative form with numerical schemes I've mentioned above.
To avoid writing a very long message i attach my code and i hope you can understand all the steps.
Now the question: do you think the plots i obtained are correct? Is that what you expect from a Lax-Wendroff scheme?
To be onest i think something in my Lax Wendroff scheme is not working because the plots I've obtained show the solution is not converging and that would mean the scheme is not stable, but it should be more stable than Lax-Friederichs one! Moreover, i expect my solution to converge or, at least, to stabilize in a little range of values.
Well, I'm sorry for my bad grammar and i hope you can help me.
Best regards.
i'm very new to the forum so i hope I've used the correct form to write my question.
Anyway, i need some help to evaluate the result of my last analysis: I'm studying the flux flowing inside an ICE aspiration manifold in a very simplified way (1D flux, ideal gas, compressible flow). For the analysis I've implemented the Matlab code for a Lax-Wendroff scheme and for a Lax-Friderichs scheme using the following assumptions:
the air aspirated in the manifold is initially in the ambient condition;
the conditions at the inlet could be find using the energy and mass conservation law that give: T1 = 293.08 K ; P1 = 95421.5 Pa ; u1 = 2.77 m/s.
the pressure value at the outlet can be found assuming the rotation speed of the engine (n = 6000 rpm) and knowing the geometry of the cylinder;
the value I've found is about 5kPa, so P2 = 90161 Pa
Now, i have to solve the mass, momentum and energy conservation in the conservative form with numerical schemes I've mentioned above.
To avoid writing a very long message i attach my code and i hope you can understand all the steps.
Now the question: do you think the plots i obtained are correct? Is that what you expect from a Lax-Wendroff scheme?
To be onest i think something in my Lax Wendroff scheme is not working because the plots I've obtained show the solution is not converging and that would mean the scheme is not stable, but it should be more stable than Lax-Friederichs one! Moreover, i expect my solution to converge or, at least, to stabilize in a little range of values.
Well, I'm sorry for my bad grammar and i hope you can help me.
Best regards.