uwochris
Flightinfo's sexiest user
- Joined
- Dec 21, 2001
- Posts
- 381
Hey guys,
I have heard contradictory statements on the relation between your prop pitch (fine vs. coarse) and TAS, and I would like some of your opinions.
I always thought that with a finer setting (high RPM), you will have a higher fuel consumption, higher temperatures for CHT, and a higher TAS. Is this the case?
Also, can someone explain when and why prop efficiency is greatest- low, or high RPM?
I understand that with a coarse setting (low RPM), the prop's AOA is greater and thus, the props take a "bigger" bite out of the air, implying greater distance travelled per revolution (i.e. pitch). I always thought this implied a higher TAS, but this is contradictory to the first statement I made. Am I misinterpreting something?
Any help is greatly appreciated.
Chris.
I have heard contradictory statements on the relation between your prop pitch (fine vs. coarse) and TAS, and I would like some of your opinions.
I always thought that with a finer setting (high RPM), you will have a higher fuel consumption, higher temperatures for CHT, and a higher TAS. Is this the case?
Also, can someone explain when and why prop efficiency is greatest- low, or high RPM?
I understand that with a coarse setting (low RPM), the prop's AOA is greater and thus, the props take a "bigger" bite out of the air, implying greater distance travelled per revolution (i.e. pitch). I always thought this implied a higher TAS, but this is contradictory to the first statement I made. Am I misinterpreting something?
Any help is greatly appreciated.
Chris.