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jsbsim.js

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JSBSim flight dynamics model ported to JavaScript

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<?xml version="1.0"?> <!-- 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>