(Solved): Consider a shear cap section attached to a spar of the box beam and imagine that upward deflection ...

Consider a shear cap section attached to a spar of the box beam and imagine that upward deflection of the wing resulting from an upward helicopter is in a stable hover. Using engineering analysis tools (EXCEL, MATLAB, CATIA, SOLIDWORKS, etc.) that you have been exposed to in range from \( 0.0 \) to 600 pounds force. Assume the given dimensions and material properties provided. In this module (part 1 ) discussion assume "L" direction properties. 1. The honeycomb cell wall thickness is \( 0.015 \) inch; the cell diameter is \( 0.25 \) inch and the height of a core cell is \( 0.50 \) inch. 2. The honeycomb material is Nomex (Aramid Fiber) and the specimen dimension are thickness \( 0.5 \) inch, width \( 1.80 \) inches, and length \( 6.0 \) inches. core sample and "goes with the pointed part" of the cell. The enlarged sample on the left is \( 1 / 4 \) " cell honeycomb that has a perity cubic foot and the other sample is a 3 -pound density with \( 1 / 8^{\prime \prime} \) cell.