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 10 lbs/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 100 psi. Calculate the maximum bending moment; and the maximum flexural/bending stress.
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 10 lbs/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 100 psi. Calculate the maximum bending moment; and the maximum flexural/bending stress.
Chapter2: Loads On Structures
Section: Chapter Questions
Problem 1P
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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 10 lbs/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 100 psi. Calculate the maximum bending moment; and the maximum flexural/bending stress.
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