PPRuNe Forums - View Single Post - Lift limit - Reducing AoA with an increase in CAS?
Thread: Lift limit - Reducing AoA with an increase in CAS?
View Single Post
Old 7th November 2011 | 10:38
  #8 (permalink)  
BOAC
Per Ardua ad Astraeus
 
Joined: Mar 2000
Posts: 18,575
Likes: 4
From: UK
"From 0.2 to 0.6 Mach you must consider compressibility." For a thickish wing section this could cause that reduction in AoA, I guess.
BOAC is offline  
Reply
0