The mean dimensions of the cross section of the leadingedge and torsion box of an airplane wing can beapproximated as shown. The wing is subjected to atorque of 4.7 MN m and the wall thickness is 10 mm.The wing is made of 2014-T6 aluminum alloy.Figure 1of 10.5 m10 mm10 mm10 mm2 m0.25 m0.25 mExpress your answer with the appropriate units.Tavg 124 MPaSubmitCorrectPart BMy Answers Give UpDetermine the angle of twist per meter length of the wing.Express your answer with the appropriate units.VΠΙ ΑΣΦ It vecSubmitMy Answers Give UpIncorrect; Try Again; 5 attempts remaining?°/m

The mean dimensions of the cross section of the leading edge and torsion box of an airplane wing can be approximated as shown. The wing is subjected to a torque of 4.7 MN m and the wall thickness is 10 mm. The wing is made of 2014-T6 aluminum alloy. Figure 1 of 1 Express your answer with the appropriate units. Tavg= 124 MPa Submit Correct Part B My Answers Give Up Determine the angle of twist per meter length of the wing.

The mean dimensions of the cross section of the leading edge and torsion box of an airplane wing can be approximated as shown. The wing is subjected to a torque of 4.7 MN m and the wall thickness is 10 mm. The wing is made of 2014-T6 aluminum alloy. Figure 1 of 1 Express your answer with the appropriate units. Tavg= 124 MPa Submit Correct Part B My Answers Give Up Determine the angle of twist per meter length of the wing.

Structural Analysis

6th Edition

ISBN:9781337630931

Author:KASSIMALI, Aslam.

Publisher:KASSIMALI, Aslam.

Chapter2: Loads On Structures

Section: Chapter Questions

Problem 1P

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The mean dimensions of the cross section of the leading edge and torsion box of an airplane wing can be approximated as shown. The wing is subjected to a torque of 4.7 MN m and the wall thickness is 10 mm. The wing is made of 2014-T6 aluminum alloy. Figure 1 of 1 0.5 m 10 mm 10 mm 10 mm 2 m 0.25 m 0.25 m Express your answer with the appropriate units. Tavg 124 MPa Submit Correct Part B My Answers Give Up Determine the angle of twist per meter length of the wing. Express your answer with the appropriate units. VΠΙ ΑΣΦ It vec Submit My Answers Give Up Incorrect; Try Again; 5 attempts remaining ? °/m
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