BiomimeticWings
Recruit
- 5
- Nov 26, 2025
Hey Guys,
I am searching for data (like offical testing results or handbooks, anything quantifieable) about the performance of Spitfire Propellors. More specifically the one used in the Seafire Mk. 47, the Spitfire Mk. 22 or the Spitfire Mk. IX. The Propellors used as I have read amongst others in this forum are propellors with the blades:
- DRG. RA.10129 (Spitfire Mk 22/24)
- DRG. RA.10270 (Seafire Mk 47)
- and the Mk. IX three bladed ones (havent found Information of exact types yet)
The picture below is an example of the kind of information I am looking for in particular.
This would be the propeller efficiency at different pitch angles at a given speed. (η_P = propellor efficiency, J = degree of advancement? (translated from german "Fortschrittsgrad")). I am sure the royal airforce has recorded data of that sorts of aircraft and propellor performance, however I coul not find any in scientific papers.
So in short:
If anybody had some information or access to handbooks, data or something similar about the propellors performance at certain pitches and speeds, as well as optimal or required revolutions at takeoff, travel, etc. and would be willing to share their information, that would help a lot.
Tank you and have a great day!
I am searching for data (like offical testing results or handbooks, anything quantifieable) about the performance of Spitfire Propellors. More specifically the one used in the Seafire Mk. 47, the Spitfire Mk. 22 or the Spitfire Mk. IX. The Propellors used as I have read amongst others in this forum are propellors with the blades:
- DRG. RA.10129 (Spitfire Mk 22/24)
- DRG. RA.10270 (Seafire Mk 47)
- and the Mk. IX three bladed ones (havent found Information of exact types yet)
The picture below is an example of the kind of information I am looking for in particular.
This would be the propeller efficiency at different pitch angles at a given speed. (η_P = propellor efficiency, J = degree of advancement? (translated from german "Fortschrittsgrad")). I am sure the royal airforce has recorded data of that sorts of aircraft and propellor performance, however I coul not find any in scientific papers.
So in short:
If anybody had some information or access to handbooks, data or something similar about the propellors performance at certain pitches and speeds, as well as optimal or required revolutions at takeoff, travel, etc. and would be willing to share their information, that would help a lot.
Tank you and have a great day!