Problem M8: Calculating Deflection of Point D in a Symmetric Truss, Exercises of Aeronautical Engineering

A problem statement for a university engineering course, unified engineering i, during the fall 2003 semester. Students are asked to calculate the deflection of point d in a truss under a given loading, using the young's modulus, cross-sectional area, and length of the bars. The document also suggests drawing a displacement diagram and comparing the results with experimental data from the truss lab. Students can assume values for l, a, and e for aluminum or steel.

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2011/2012

Uploaded on 07/22/2012

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Unified Engineering I Fall 2003
Problem M8 (Materials and Structures)
For the truss shown below (and analyzed in M7) calculate the deflection of point D under the
loading shown. The bars have length L or √2L and all angles are either 90° or 45°. The bars
have cross-sectional area A and they are made of a material with Young’s modulus E. Hint,
draw a displacement diagram starting at points E and D – what can you say about the
displacement of D relative to E given that this is a symmetric structure?.
Since this is the truss that you are experimenting with in the truss lab, you can also compare
the results of the experiments to the analysis. By assuming values for L, A and E (70 GPa for
aluminum, 210 GPa for steel) estimate the relationship between applied load and the
deflection of point D for the experimental truss and compare with your data. If the two
results are not similar, suggest potential reasons for the discrepancy.
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Unified Engineering I Fall 2003 Problem M8 (Materials and Structures) For the truss shown below (and analyzed in M7) calculate the deflection of point D under the loading shown. The bars have length L or √2L and all angles are either 90° or 45°. The bars have cross-sectional area A and they are made of a material with Young’s modulus E. Hint , draw a displacement diagram starting at points E and D – what can you say about the displacement of D relative to E given that this is a symmetric structure?.

Since this is the truss that you are experimenting with in the truss lab, you can also compare the results of the experiments to the analysis. By assuming values for L, A and E (70 GPa for aluminum, 210 GPa for steel) estimate the relationship between applied load and the deflection of point D for the experimental truss and compare with your data. If the two results are not similar, suggest potential reasons for the discrepancy.

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