structures4 - 10.1 10 33.05 1113.03 y Shear Force N Bending...

Info iconThis preview shows page 1. Sign up to view the full content.

View Full Document Right Arrow Icon
y Elliptical c(y) Wing Chord Average Chord Strip Strip Area Lift on each strip 0 23.67 20.2 21.94 1 71.77 2417.26 3.64 23.52 20.2 21.86 2 71.53 2409.16 7.28 23.08 20.2 21.64 3 70.8 2384.57 10.92 22.31 20.2 21.26 4 69.55 2342.48 14.56 21.2 20.2 20.7 5 67.73 2281.01 18.2 19.67 20.2 19.94 6 65.23 2196.88 21.84 17.63 20.2 18.91 7 61.88 2084.19 25.48 14.85 20.2 17.52 8 57.34 1931.25 29.12 10.79 20.2 15.5 9 50.71 1707.77 32.72 0 20.2
Background image of page 1
This is the end of the preview. Sign up to access the rest of the document.

Unformatted text preview: 10.1 10 33.05 1113.03 y Shear Force, N Bending Momen, N*m 20867.6 37979.03 3.64 18450.34 100738.86 7.28 16041.18 145974.73 10.92 13656.61 173985.24 14.56 11314.13 185325.49 18.2 9033.12 180843.04 21.84 6836.24 161745.49 25.48 4752.05 129730.96 29.12 2820.8 87219.08 32.72...
View Full Document

Ask a homework question - tutors are online