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 wlc 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 vertical reactions of the two hinges. (Check all correct answers) * Bv = 300 lb downward Bv = 600 lb downward Av = 0 Av = 600 lb upward Bv = 600 lb upward Av = 300 lb upward Av = 600 lb downward Av = 300 lb downward Bv = 0 Bv = 300 lb upward

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 wlc 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 vertical reactions of the two hinges. (Check all correct answers) * Bv = 300 lb downward Bv = 600 lb downward Av = 0 Av = 600 lb upward Bv = 600 lb upward Av = 300 lb upward Av = 600 lb downward Av = 300 lb downward Bv = 0 Bv = 300 lb upward