PLEASE WRITE IN OCTAVE PROGRAMMING LANGUAGE TO SOLVE THIS PROBLEM Problem 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. BELOW IS EXPLANATION FOR THE IMAGE:   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. τ = P/A0sinθcosθ Where A0 is the cross sectional area perpendicular to the long axis of the block and θ is the angle formed by the normal (perpendicular) plane and the oblique plane.

Computer Networking: A Top-Down Approach (7th Edition)
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Author:James Kurose, Keith Ross
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PLEASE WRITE IN OCTAVE PROGRAMMING LANGUAGE TO SOLVE THIS PROBLEM

Problem

  • 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.

BELOW IS EXPLANATION FOR THE IMAGE:

 

The 1.4-kip load 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.

τ = P/A0sinθcosθ

Where A0 is the cross sectional area perpendicular to the long axis of the block and θ is the angle formed by the normal (perpendicular) plane and the oblique plane.

5.0 in.
3.0 in.
60°
P'
Transcribed Image Text:5.0 in. 3.0 in. 60° P'
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