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Old 12-11-2012, 01:18 PM
taildraggernut taildraggernut is offline
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Quote:
Originally Posted by Crumpp View Post
At the forward CG point where our elevator requires the most moment, the airplane should not spin. As the CG moves rearward, the ability to enter a spin is increased until at its most rearward position a spin entry is possible with deliberate effort.
So basically you aknowlege the RAE evaluation that the aircraft was 'too stable' for a fighter, if you are having to use up elevator effect simply to counter the CoG then you have afairly impeded manouverability.