PPRuNe Forums - View Single Post - Aft fuselage mounted engines and static longitudinal stability
Old 1st September 2010 | 19:38
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Dick Whittingham
 
Joined: Oct 2000
Posts: 461
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From: Bristol
This is a bit complex, and I would like an expert contribution if possible.

A cylinder shape set at an angle of attack generates a nose up moment, and this increases with increasing apha, making it an unstable couple. The plan area of the engines, stub mountings and so on acts like an extra horizontal tail, which is a stabilizing effect.

I understand that the JAA answer is that on balance the total efect comes out stable

Dick
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