Nordy
03-11-2006, 12:18 PM
Hello,
first as a newcomer I send greeting to all here.
I'm very interested in propeller physics and have created some formulas for thrust and torque to calculate speed of small gliding boats.
I use the wellknown formulas for thrust and torque and the wageningen b-series kt and kq coefficients.
Assuming kt and kq are linear around the max-speed point you can easily find two steady state formulas.
The thrust formula finds the needed advance ratio with respect to kt and kq latter depending on prop geometry (diameter, pitch/diameter ratio , blade number and expanded area ratio).
The torque formula delivers the needed engine revolution assuming a linear engine torque dependance.
In the case of optimizing a given prop you always know boat's speed and revolution you aren't satisfied with.
Ideally you know two boat and engine speeds, one for light and one for heavy loaded boat.
This has the big advantage you'll know the driving resistance of your boat and put it into the formula.
And you have some other boundary conditions for kt and kq to reach the performed speeds in calculation.
What you further must know is easy to have, outboard engine power at prop wheel and max power engine speed, gear ratio, propeller diameter, pitch, blade number and expanded area.
The third order b-series kt and kq polynomials and the formulas for thrust, torque, resistance and so on are caculated by excel.
All works well.
But I have the problem, calculated values of v max and n max are always too low.
A typical example:
A 5,50m rib reaches in practice 60 km/h, the engine speed is 5800.
The calculated speeds are 56 km/h and 5600 rpm.
The prop efficiency J/2Pi*Kt/kq is 79%, that's a common and very good value almost at the limit.
If I apply kt and kq multipliers to let the two formulas fulfill the boundaries (60km/h and 5800 rpm) the efficiency will rise to impossible 95 or more per cent.
Nevertheless varying prop geometry then will bring very reasonable results.
I understand the used prop will always differ from the B-series type and boat conditions differ as well from the wageningen free water test field.
That's why kt and kq multipliers will always have to be applied.
But I don't understand why it takes a 95 % or better efficiency to reach the performed speeds.
In some calculations I had the perpetuum mobile (Eta > 100%) !?
Has anybody an idea ?
Best greetings from snowy Germany
Peter
first as a newcomer I send greeting to all here.
I'm very interested in propeller physics and have created some formulas for thrust and torque to calculate speed of small gliding boats.
I use the wellknown formulas for thrust and torque and the wageningen b-series kt and kq coefficients.
Assuming kt and kq are linear around the max-speed point you can easily find two steady state formulas.
The thrust formula finds the needed advance ratio with respect to kt and kq latter depending on prop geometry (diameter, pitch/diameter ratio , blade number and expanded area ratio).
The torque formula delivers the needed engine revolution assuming a linear engine torque dependance.
In the case of optimizing a given prop you always know boat's speed and revolution you aren't satisfied with.
Ideally you know two boat and engine speeds, one for light and one for heavy loaded boat.
This has the big advantage you'll know the driving resistance of your boat and put it into the formula.
And you have some other boundary conditions for kt and kq to reach the performed speeds in calculation.
What you further must know is easy to have, outboard engine power at prop wheel and max power engine speed, gear ratio, propeller diameter, pitch, blade number and expanded area.
The third order b-series kt and kq polynomials and the formulas for thrust, torque, resistance and so on are caculated by excel.
All works well.
But I have the problem, calculated values of v max and n max are always too low.
A typical example:
A 5,50m rib reaches in practice 60 km/h, the engine speed is 5800.
The calculated speeds are 56 km/h and 5600 rpm.
The prop efficiency J/2Pi*Kt/kq is 79%, that's a common and very good value almost at the limit.
If I apply kt and kq multipliers to let the two formulas fulfill the boundaries (60km/h and 5800 rpm) the efficiency will rise to impossible 95 or more per cent.
Nevertheless varying prop geometry then will bring very reasonable results.
I understand the used prop will always differ from the B-series type and boat conditions differ as well from the wageningen free water test field.
That's why kt and kq multipliers will always have to be applied.
But I don't understand why it takes a 95 % or better efficiency to reach the performed speeds.
In some calculations I had the perpetuum mobile (Eta > 100%) !?
Has anybody an idea ?
Best greetings from snowy Germany
Peter