With the increase in Altitude, keeping the IAS constant TAS increases as Density decreases. With decrease in Density, the performance of an aircraft decreases. Thus, at same attitude, to keep same IAS an aircraft would need to produce more thrust.
Would the throttle or power settings needs to be increased?
What effect is dominant on Fuel Consumption, Power or Density?
Would the throttle or power settings needs to be increased?
What effect is dominant on Fuel Consumption, Power or Density?