PPRuNe Forums - View Single Post - Aft fuselage mounted engines and static longitudinal stability
Old 2nd September 2010 | 20:11
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manucordier
 
Joined: Aug 2010
Posts: 122
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From: Brussels
the rear of the fuselage eng. -> less influence of thrust change

Thanks a lot for you explicite and brief answers.

I have another question about rear fuselage mounted engines.
I've read that an advantage of locating the engines at the rear of the fuselage, in comparison to a location beneath the wing is less influence of thrust change.

Well I have been thinking about that, reading literature... and truly I don't understand why.

If you can help me with that one I would be grateful.

Have a good night,
Emmanuel Cordier.
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