Consider one wing aileron w/ rectangular planform. This aileron w/ constant chord has a span of ó ft & a uniform spanwise air load distribution of 10 lbs/ft. It is supported by two hinges wic are located at the tips of the span. The air loading is assumed to be transmitted to a single spar wic is connected at the tips to the wing. The cross-section of the spar is constant throughout the aileron span. Calculate the vertical reactions of the two hinges. (Check all correct answers) *

Consider one wing aileron w/ rectangular planform. This aileron w/ constant chord has a span of ó ft & a uniform spanwise air load distribution of 10 lbs/ft. It is supported by two hinges wic are located at the tips of the span. The air loading is assumed to be transmitted to a single spar wic is connected at the tips to the wing. The cross-section of the spar is constant throughout the aileron span. Calculate the vertical reactions of the two hinges. (Check all correct answers) *

International Edition---engineering Mechanics: Statics, 4th Edition

4th Edition

ISBN:9781305501607

Author:Andrew Pytel And Jaan Kiusalaas

Publisher:Andrew Pytel And Jaan Kiusalaas

Chapter9: Moments And Products Of Inertia Of Areas

Section: Chapter Questions

Problem 9.60P: Determine Iu for the inverted T-section shown. Note that the section is symmetric about the y-axis.

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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 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.* 450 psi - 450 psf 45 psf - 45 psi - 450 psi 450 psf - 45 psf 45 psi
Consider one wing aileron w/ a 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. If the front area of the aileron is circular in cross-section w/ radius of 1 in., determine the reactions of the supports w/ their proper directions. (Select two correct answers)
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is this truss statically deteriminant or indeterminant
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Classwork Problem 3 A cantilever beam 2m span carries point loads as shown. Draw the shear force and bending moment diagrams. The self weight of the beam is 400N 300 N 500 N 800 N 0.5 m- 0.7 m 0.8 m 13
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