Hi I have this question that I need the explanation to if possible
An a/craft has a gradient of 3.3% flying at IAS of 85knts at a pressure Alt of 8000ft temp 15 degrees will have a rate of climb of ??
I have the answer of 334Ft/Min
What is the formula to get there?
I have tried ROC= V sin Y but do not get 334
I need someone to help me see how to get to this figure.
Cheers