5. A metallic top-hat stringer reinforced wing skin (function of the material A=150) has a width of 1.5 m and an unsupported length of 0.5 m. If the applied compressive load is 120
5. A metallic top-hat stringer reinforced wing skin (function of the material A=150) has a width of 1.5 m and an unsupported length of 0.5 m. If the applied compressive load is 120
Chapter2: Loads On Structures
Section: Chapter Questions
Problem 1P
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![5. A metallic top-hat stringer reinforced wing skin (function of the material Ã=150) has a
width of 1.5 m and an unsupported length of 0.5 m. If the applied compressive load is 120
kN, then calculate the allowable bending stress %. If we assume that the stringers cross-
section area is 50% of skin panel cross-section area, and the ultimate bending moment is
150 kN•m, then determine the equivalent and minimum skin thickness, and t, for the
wing box with an average depth of h=0.3m, according to this ultimate bending moment.](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2F5f7fd42a-4300-4da8-8f14-b18670105553%2F16b74877-a7b6-4014-8967-c157bce258ec%2Fayowvzc_processed.png&w=3840&q=75)
Transcribed Image Text:5. A metallic top-hat stringer reinforced wing skin (function of the material Ã=150) has a
width of 1.5 m and an unsupported length of 0.5 m. If the applied compressive load is 120
kN, then calculate the allowable bending stress %. If we assume that the stringers cross-
section area is 50% of skin panel cross-section area, and the ultimate bending moment is
150 kN•m, then determine the equivalent and minimum skin thickness, and t, for the
wing box with an average depth of h=0.3m, according to this ultimate bending moment.
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