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...
During Development state of helicopters, some reduction for load spectrum is generally applied?
Someone told me that normal procedure is applying some reduction of spectrum before flight test to make it easer to analyze.
But, I'm not sure that this is general procedure or not.
I feel more...