I have a problem with the cp location in xflr5.On condition that the angle of attack increases, the cp location will come to near the front side of the wing, but in my program, the cp location does not come to the front side of the wing on the contrary my cp location goes backward.
While doing stability analysis on xflr5 I'm facing some errors that's why the modes for longitudinal and lateral stability are not operating could you plz guide me through this? Like which parameters should I consider for generating the view of root locus graph. It would be a huge favour if u could help me out
While doing stability analysis on xflr5 I'm facing some errors that's why the modes for longitudinal and lateral stability are not operating could you plz guide me through this?
so proud to see this knowledge comes from arab country !!! appreciate it a lot thanks man
Great video! Please enable youtube auto subtitles
thank you!! it helped in my project.
great explaination sir!
I have a problem with the cp location in xflr5.On condition that the angle of attack increases, the cp location will come to near the front side of the wing, but in my program, the cp location does not come to the front side of the wing on the contrary my cp location goes backward.
what is control parameter, why you took its value from 0 to 1
While doing stability analysis on xflr5 I'm facing some errors that's why the modes for longitudinal and lateral stability are not operating could you plz guide me through this?
Like which parameters should I consider for generating the view of root locus graph. It would be a huge favour if u could help me out
While doing stability analysis on xflr5 I'm facing some errors that's why the modes for longitudinal and lateral stability are not operating could you plz guide me through this?
Why did you put a 2 kg mass in the point -10m (instead of -0.010 m). Thats changes Cm and the whole calculations and makes them false