08-05-2012, 12:28 AM
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Approved Member
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Join Date: Feb 2008
Posts: 1,552
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The worst case scenario means here a Rotol propeller and CoG behind the aft limit for that configuration, like in the NACA tested Spitfire.
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Fixed Pitch Wooden Airscrew
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Longitudinally, the aircraft is stable with centre of gravity forward, but is unstable with centre of gravity normal and aft with engine 'OFF' and 'ON'. Longitudinal stability records are attached.
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http://www.spitfireperformance.com/k9787-fuel.html
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