jsbsim.js
Version:
JSBSim flight dynamics model ported to JavaScript
126 lines (118 loc) • 2.06 kB
text/xml
<!-- Generated by Java Prop
Inputs:
Diameter D 4.66 [m]
Spinner Dia. Dsp 2.3 [m]
Speed of Rotation n 2500 [1/min]
Velocity v 200.000 [m/s]
Number of Blades B 6 [-]
square tip
Outputs:
v/(nD) 1.03 v/(OR) 0.328
Efficiency ? 85.776 % loading low
Thrust T 17,584.13 N Ct 0.0176
Power P 4,099.99 kW Cp 0.0211
B at 75%R 27.1 Pitch H 5.61 m
v/(nD) 1.03 v/(OR) 0.328
Efficiency ? 85.776 % loading low
Thrust T 17,584.13 N Ct 0.0176
Power P 4,099.99 kW Cp 0.0211
B at 75%R 27.1 Pitch H 5.61 m
static thrust (kN):25.38
-->
<propeller name="prop">
<ixx> 7.9504 </ixx>
<diameter unit="IN"> 183.5 </diameter>
<numblades> 6 </numblades>
<gearratio>1.00 </gearratio>
<table name="C_THRUST" type="internal">
<tableData>
0.00 0.038163
0.05 0.045115
0.10 0.046475
0.15 0.045026
0.20 0.044015
0.25 0.043101
0.30 0.042092
0.35 0.041006
0.40 0.039864
0.45 0.038708
0.50 0.037681
0.55 0.036689
0.60 0.035682
0.65 0.034650
0.70 0.033574
0.75 0.033193
0.80 0.032219
0.85 0.030209
0.90 0.027452
0.95 0.023779
1.00 0.019926
1.05 0.016033
1.10 0.012099
1.11 0.011307
1.12 0.010513
1.13 0.009718
1.14 0.008921
1.15 0.008121
1.16 0.007319
1.17 0.006517
1.18 0.005712
1.19 0.004904
1.20 0.004083
1.21 0.003258
1.22 0.002424
1.23 0.001605
1.24 0.000783
1.25 -0.000051
1.26 -0.000885
1.27 -0.001719
1.28 -0.002553
1.29 -0.003387
1.30 -0.004221
</tableData>
</table>
<table name="C_POWER" type="internal">
<tableData>
0.00 0.038939
0.05 0.044732
0.10 0.045131
0.15 0.043421
0.20 0.042548
0.25 0.041868
0.30 0.041205
0.35 0.040582
0.40 0.040017
0.45 0.039394
0.50 0.038678
0.55 0.038334
0.60 0.037981
0.65 0.037702
0.70 0.037267
0.75 0.034058
0.80 0.032719
0.85 0.031415
0.90 0.029491
0.95 0.026607
1.00 0.023278
1.05 0.019629
1.10 0.015659
1.11 0.014826
1.12 0.013981
1.13 0.013124
1.14 0.012254
1.15 0.011371
1.16 0.010476
1.17 0.009571
1.18 0.008654
1.19 0.007728
1.20 0.006781
1.21 0.005827
1.22 0.004856
1.23 0.003893
1.24 0.002919
1.25 0.001919
1.30 -0.003081
</tableData>
</table>
</propeller>