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Matching the Lift in order to calculate the flap angle

- May 24, 2023 at 10:18 am
  
  marco.peviani
  Subscriber
  
  Hi everyone, I have a NACA 4410 profile which I have done an analysis at different AoA (parameterizing the AoA) to find the CL and the CD. Now I want another run but with a 2410 with flaps, matching the lift from the first analysis to get the flap angle to have the same LIft.
  For example I have the 4410 at 5° of AoA and I find that the CL is 0.93, now with the same CL I want to find the Flap angle (of 2410).
  How can I do ?
  Thanks in advance
- May 24, 2023 at 12:43 pm
  
  Federico
  Ansys Employee
  
  Hello Marco,
  you can set up a parametric simulation with the AoA as your parameter using Workbench. Set a range values expected for the AoA and run through these points until you approach the desired value.
  Working with Parameters and Design Points (ansys.com)
- May 24, 2023 at 12:51 pm
  
  marco.peviani
  Subscriber
  
  Thanks for the reply, but my problem is related to the matching of the CL without going to trial and error also because for this project I have to do various simulations and it would take a lot. Would it be possible to have AoA as output variable matching the CL?

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