Structural Testing Of Homebuilt Aircraft
element, 23.9% for the next, etc. We entire board's length. There may be extent. Numerous wind tunnel investi-
use the same interpolation method if complications here if, for example, we gations tend to confirm this, especially
our wing has an AR between those have heavy fuel tanks sitting at the when proper wing fairings have been
printed in the Table. We now have 6 wing tips, or wing-mounted engines, installed. We will simply assume that
"packages" representing the entire but these cases are beyond our pre- no mistake is made if we extend the
half-wing lift - all 100% of it. All we sent discussion. The de-signer has wing loading across the fuselage as if
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