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Thread: Effect of CP on aircraft pitch attitude
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Old 20th Feb 2017, 21:46
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FE Hoppy
 
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I agree in the flaps extended case but I'm sure I've seen lower Cl on flap 0 + slat vs no slat.

Remember we are talking about off design geometry following a flap failure.

Here is an old but interesting report.
http://naca.central.cranfield.ac.uk/...ca-tn-3129.pdf
Last edited by FE Hoppy; 20th Feb 2017 at 22:01. Reason: added link
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