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Re: Whitley test "produced a failure at 98% of the design load" is that good?
Don't ask me for a reference, but I seem to recall asymmetric loading being discussed at the university level in pre-war papers. (The classic rolling pull-up.) Whether it had made its way into RAF requirements is another question.
In today's terms, ultimate load can be 150% design load or 150% service load. As I said, without knowing more it is hard to draw firm conclusions about this test result.
And I have had more than one boss who would tell you that failure at 102% meant the @#$%& thing was too heavy!
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