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Hello
I need some help with prop thrust ( I think) The AC is a single engine prop. Here is what should happens with my plane :
- take-off at 90-100km/h, 2750rpm, 120kPa MP
- flaps up, acceleration to 140km/h at 2600rpm, 100kPa
- climb with 140km/h, +2m/s
- cruise 160-170km/h, 2350rpm, 80kPa
Here is what happens :
- take-off at 90-100km/h, 2750rpm, 120kPa MP
- flaps up, acceleration to 170 km/h at 2600rpm, 100kPa
- climb with 170-180 km/h, +2m/s
- cruise : slow down to 160km/h 2350rpm, 80kPa
I checked the parameters with AFSD. At T/O power the prop thrust is approx. 450kg ( I think it is too much), at cruise it drops below 200kgs. So I'm pretty sure that I have to adjust prop thrust somehow. Which table need to tweak with ? Or how can I adjust it?
I need some help with prop thrust ( I think) The AC is a single engine prop. Here is what should happens with my plane :
- take-off at 90-100km/h, 2750rpm, 120kPa MP
- flaps up, acceleration to 140km/h at 2600rpm, 100kPa
- climb with 140km/h, +2m/s
- cruise 160-170km/h, 2350rpm, 80kPa
Here is what happens :
- take-off at 90-100km/h, 2750rpm, 120kPa MP
- flaps up, acceleration to 170 km/h at 2600rpm, 100kPa
- climb with 170-180 km/h, +2m/s
- cruise : slow down to 160km/h 2350rpm, 80kPa
I checked the parameters with AFSD. At T/O power the prop thrust is approx. 450kg ( I think it is too much), at cruise it drops below 200kgs. So I'm pretty sure that I have to adjust prop thrust somehow. Which table need to tweak with ? Or how can I adjust it?
