iCLEAN â Loitering Attack UCAV - aero.com
iCLEAN â Loitering Attack UCAV - aero.com
iCLEAN â Loitering Attack UCAV - aero.com
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PIVOT STRESS CALCULATIONS AND ANALYSISSTRESS CALCULATIONSAccording to evaluate the stresses applied on the pivot:Forces and moments distribution on trapeze wing: Triangular wing distribution(Resultant force on one third of the wing) Force causes a bending moment on the wing's root. Root moment as referred as a couple of forces on the pivot.As we can achieve from stresses analysis calculations -The applied stresses are lower than the allowed stresses:122.3[ MPa] 706.3fibersallowedCarbon fibersMPa MPa16 allowed270.8Al . 7075T6hingeMPa22
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