Quote:
Originally Posted by Soren  Read the report again.
The F4U's wing stalls at 18 deg, while the P-51's stalls at 17.7 deg. |
It is well possible that I missed things and thus may be wrong but judging from this and other observations You made on technical reports, I think You are mixing it up and this comment may be filed down along Your comments about LE-slats and airfoil thickness=lift equitations. The P-51 wing (exactly an P-51B full scale model beeing tested, noted as airplane 1) doesn´t stall at 17.7 deg. You are free to verify this on Your own.
In the figures produced by the report, You can see that the wing dos provide lift at over 20 deg., when other wings are long completely stalled.
Linear Mode
