| Flight - Hovering: |
| Momentum Method |
| Disk Loading: [DL] | 1.27 | lb/ft2 |
| Velocity: [V1hov] (Average of velocities through the disk.) | 16.36 | ft/sec. |
| Power; [P] (see *) (Figure of Merit set to 0.65) | 22.24 | hp. |
| Power Loading: [PL] (for hover ONLY) (see *) | 21.76 | . | lb/hp |
| Nondimensional Coefficients; |
| Thrust: [CT] | 0.00143 |
| Power: [CP] | 0.00000 |
| CT / Sigma | 0.04379 |
| Combined Momentum and Blade Element Theory w/ Emphirical Corrections |
| Coefficients of:- |
| Thrust: [CTntl] (w/o tip loss) | 0.00135 |
| Tip loss factor: [B] | 0.97 |
| Thrust: [CT] (with tip loss) | 0.00113 |
| Profile; [CQo] | 0.00113 |
| Induced: [CQi] | 0.00004 |
| Torque: [CQ] | 0.00006 |
| Disk loading: [DL] (calculated using thrust) | 1.0126 | lb/ft2 |
| Thrust Solidity: [CT/Sigma] | 0.03483 |
| [(DL)(CT/Sigma)] | 0.03527 |
| Measured power / Calculated power | 0.96 |
| CQ / Sigma | 0.00185 |
| Thrust: [T] (see *) | 384.93 | lb |
| Horsepower: [hp] (see *) | 22.78 | hp |
| * Calculated values are at International Standard Atmosphere (i.e. Sea level & 59 deg F.). |
| Flight - Vertical: |
| Momentum Method |
| Velocity: [V1ver] (Average of velocities through the disk.) | 21.05 | ft/sec. |
| Change in power; [DeltaP] | 11.46 | hp. |
| Change in blade pitch; [DeltaTheta] | 0.03 | deg. |
| Combined Momentum and Blade Element Theory w/ Emphirical Corrections |
| Not done. |
| Flight - Forward: |
| Momentum Method |
| Velocity: [V1fwd] (Average of velocities through the disk.) | 4.85 | ft/sec. |
| Change in Power: |
| Induced: [HPind] | 4.28 | hp. |
| Parasite: [HPp] (no value included) | 0.00 | hp. |
| Profile: [HPOH] | 12.77 | hp. |
| Main (sub total): [HPm] | 17.06 | hp. |