An aircraft includes a fuselage having a nose end and a tail end and a center of gravity. A primary wing is coupled to the fuselage aft of the center of gravity. A secondary wing is coupled to the fuselage forward of the center of gravity. A v-tail is coupled to the fuselage between the primary wing and the tail end of the fuselage, the v-tail comprising first and second angled stabilizers, each of the first and second stabilizers including a first end fixed to the fuselage and a second free end, distal to the fuselage.
LIGHT TWIN ENGINE AIRCRAFT
2020-10-01
Patent
Electronic Resource
English
Engine Failure in Light Twin-Engine Aircraft
Emerald Group Publishing | 1980
ALTAU: Twin Engine Unmanned Aircraft
British Library Conference Proceedings | 2014
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