3.0 in. 60° 5.0 in. The 1.4-kip load P is supported by two wooden members of uniform cross section that are joined by the simple glued scarf splice shown. Determine the shearing stresses in the glued splice. T-sin cos 0 Where Ao is the cross sectional area perpendicular to the long axis of the block and is the angle formed by the normal (perpendicular) plane and the oblique plane. Problem (Use Octave) Prompt the user for cross-sectional dimensions, applied load, P, and material type (steel or aluminum), and splice angle. • Report back to the user whether or not the object will fail in shear. Note: Tmax for steel is 30000 psi and Tmax for aluminum is 20000 psi Screenshot your octave window with the program and output for P = 100kip, L=1.5in, W=1.5in and theta = 45 degrees, and submit it in Canvas.

3.0 in. 60° 5.0 in. The 1.4-kip load P is supported by two wooden members of uniform cross section that are joined by the simple glued scarf splice shown. Determine the shearing stresses in the glued splice. T-sin cos 0 Where Ao is the cross sectional area perpendicular to the long axis of the block and is the angle formed by the normal (perpendicular) plane and the oblique plane. Problem (Use Octave) Prompt the user for cross-sectional dimensions, applied load, P, and material type (steel or aluminum), and splice angle. • Report back to the user whether or not the object will fail in shear. Note: Tmax for steel is 30000 psi and Tmax for aluminum is 20000 psi Screenshot your octave window with the program and output for P = 100kip, L=1.5in, W=1.5in and theta = 45 degrees, and submit it in Canvas.

C++ for Engineers and Scientists

4th Edition

ISBN:9781133187844

Author:Bronson, Gary J.

Publisher:Bronson, Gary J.

Chapter7: Arrays

Section7.5: Case Studies

Problem 15E

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