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?
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?
