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JSBSim Thrusters: Difference between revisions
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→C_THRUST and C_POWER tables
| Line 173: | Line 173: | ||
Relevant formulas relating the variables in the tables: | Relevant formulas relating the variables in the tables: | ||
* Thrust: T = Ct | * Thrust: T = Ct * rho * n^2 * D^4 | ||
* Power: P = Cp | * Power: P = Cp * rho * n^3 * D^5) | ||
* Advance Ratio: J = v/(n*D) | * Advance Ratio: J = v/(n*D) | ||
* Efficiency: eta = Ct/Cp * v/(n*D) (or equivalently, Ct/Cp*J) | * Efficiency: eta = Ct/Cp * v/(n*D) (or equivalently, eta = Ct/Cp * J ) | ||
In the formulas | In the formulas | ||