So, Keith, if I follow, can you confirm then that you saying that climb GRADIENT at min drag, flat rated, will decrease (slightly) as temp increases
And if so, then can you make a determination on the climb RATE as temp increases, same conditions?
Do the perfomance charts show this climb gradient decrease as temp increases? Boeing/airbus, or both?
Do typical hi bypass engines have enough of a thrust decrease to show this decrease in climb gradient?
many thanks for your time. Your last post must have taken a considerable amount of time. Well done?