Consider one wing aileron w/ rectangular planform. This aileron w/ constant chord has a span of 6 ft & a uniform spanwise air load distribution of 100 Ibs/ft. It is supported by two hinges w/c are located at the tips of the span. The air loading is assumed to be transmitted to a single spar w/c is connected at the tips to the wing. The cross-section of the spar is constant throughout the aileron span & rectangular in shape measuring 12 inches high by 5 inches wide w/ a maximum allowable bending stress of 1000 psi. Calculate the absolute maximum bending stress.* O 450 psi O - 450 psf O 45 psf - 45 psi - 450 psi 450 psf O - 45 psf O 45 psi

Consider one wing aileron w/ rectangular planform. This aileron w/ constant chord has a span of 6 ft & a uniform spanwise air load distribution of 100 Ibs/ft. It is supported by two hinges w/c are located at the tips of the span. The air loading is assumed to be transmitted to a single spar w/c is connected at the tips to the wing. The cross-section of the spar is constant throughout the aileron span & rectangular in shape measuring 12 inches high by 5 inches wide w/ a maximum allowable bending stress of 1000 psi. Calculate the absolute maximum bending stress.* O 450 psi O - 450 psf O 45 psf - 45 psi - 450 psi 450 psf O - 45 psf O 45 psi

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

Section: Chapter Questions

Problem 1.1MA

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