DYNAMICS OF MACHINES AND VEHICLES
Solution
Part 1 – Dynamic Modelling
Expand space as appropriate.
Part 2 – Dynamic Analysis and Computation
Transient solution of MDOF Wing Structure:
Imported figures of the displacement response obtained using your version of owncode.m should be shown below:
Figure 1 Response at Wing Centre
Figure 2 Response at Wing Tip
Cut and paste (or print) numerical values of your matrices [m] and [k] below:
NATURAL FREQUENCIES (rad/sec) (in ascending order)
w1 =
w2 =
w3 =
w4 =
w5 =
w6 =
w7 =
MODAL MATRIX
MODAL DAMPING FACTORS xi UNDAMPED MODAL NATURAL FREQUENCIES wni
x1 = w1 =
x2 = w2 =
x3 = w3 =
x4 = w4 =
x5 = w5 =
x6 = w6 =
x7 = w7 =
p(4)
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