Structural Testing Of Homebuilt Aircraft
80 %
compose after all measurements have wait for the buckling to disappear.
been completed, the position of the This buckling, if it appears over the
"virgin" wing is shown as (0) and the glued areas (over the main and auxil-
position at the 10%-20%, in our iary spar, ribs), can signal poor
example wing 19.8%, is shown as bonding. We make notes about that,
point (1). On the horizontal axis we hold a brief conference and decide
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