Anyhow, CL, CD or Cwhatever values mean absolutely NOTHING if reference surface (and reference length for couple of forces) is unknown. Anybody with basic notions in aerodynamics should know this. I can announce CL values of 1700 for a brick if I just select a reference surface small enough if I wish to do so and nobody could claim me wrong.
The CL values in this report are only interesting in relative terms with respect to different flap angles.
Last edited by 41Sqn_Stormcrow; 06-01-2012 at 11:17 PM.
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06-01-2012, 11:13 PM
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