SentryIP
Better lucky than good!
- Joined
- Dec 9, 2001
- Posts
- 223
Hello All,
I've been told that the center-of-gravity location of an airplane affects the stall speed. This is news to me. I'm talking about a conventional airplane with positive static stability and not a fly-by-wire airplane with relaxed static stability. I know that the stall speeds vary due to altitude, gross weight, configuration and bank angle and the only way an airplane can stall is by exceeding the CLmax angle-of-attack. This person is telling me that an airplane with a center-of-gravity near the aft limit will stall at a slower airspeed than an airplane with the center-of-gravity near the forward limit. Does this person know something I don't know? If you respond, can you please give the reference you used? Thanks in advance.
I've been told that the center-of-gravity location of an airplane affects the stall speed. This is news to me. I'm talking about a conventional airplane with positive static stability and not a fly-by-wire airplane with relaxed static stability. I know that the stall speeds vary due to altitude, gross weight, configuration and bank angle and the only way an airplane can stall is by exceeding the CLmax angle-of-attack. This person is telling me that an airplane with a center-of-gravity near the aft limit will stall at a slower airspeed than an airplane with the center-of-gravity near the forward limit. Does this person know something I don't know? If you respond, can you please give the reference you used? Thanks in advance.