Effect of TIT, CPR, TAS and altitude
3 important questions on Effect of TIT, CPR, TAS and altitude
The performance(specific Thrust& TSFC) is effected by?
TIT+ CPR(properties of the engine) Ca+ h(properties of the aircraft)
Altitude increase--> thrust reduces تدريجيا
why?
Density decreases, so the engine has less air to accelerate.
we need less air at higher altitudes so no problem
we need less air at higher altitudes so no problem
What is flat rating temperature?
Thrust is keeping at a constant level
The question on the page originate from the summary of the following study material:
- A unique study and practice tool
- Never study anything twice again
- Get the grades you hope for
- 100% sure, 100% understanding
Remember faster, study better. Scientifically proven.
