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Application of Load Factor requirement of ADS29?

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darkaerie

New member
Dec 21, 2006
2
ADS29 and Mil-s-8698 requires vertical limit load factor of 3.5g on BSDGW.

BSDGW would be primary mission weight.
But 3.5g is not a demonstration condition during flight test.
And also for the utility helicopters, it seems not a realistic conditions.

How can I analyze 3.5g at BSDGW for the helicopters which has lower lift capability than 3.5g?

 
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