3390000b98
two-blade aluminum prop (provided to Jon by Hartzell) + 10% for the engine (at Jon's suggestion).
66 lines
2.7 KiB
XML
66 lines
2.7 KiB
XML
<?xml version="1.0"?>
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<FG_PROPELLER NAME="Clark Y 0.08 thickness/chord ratio variable pitch">
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IXX 1.8
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DIAMETER 84
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NUMBLADES 2
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MINPITCH 11
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MAXPITCH 27
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MINRPM 700
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MAXRPM 2700
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C_THRUST 26 5
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11.0 15.0 19.0 23.0 27.0
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0.10 0.0700 0.0815 0.0798 0.0877 0.0990
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0.15 0.0654 0.0802 0.0828 0.0871 0.0963
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0.20 0.0603 0.0782 0.0841 0.0864 0.0940
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0.25 0.0547 0.0761 0.0849 0.0855 0.0917
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0.30 0.0488 0.0716 0.0838 0.0845 0.0896
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0.35 0.0420 0.0666 0.0815 0.0831 0.0875
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0.40 0.0350 0.0605 0.0775 0.0817 0.0855
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0.45 0.0278 0.0545 0.0725 0.0802 0.0838
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0.50 0.0206 0.0470 0.0677 0.0788 0.0819
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0.55 0.0130 0.0382 0.0615 0.0770 0.0805
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0.60 0.0056 0.0297 0.0545 0.0739 0.0800
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0.65 -0.0010 0.0218 0.0427 0.0696 0.0795
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0.70 -0.0010 0.0139 0.0398 0.0640 0.0779
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0.75 -0.0010 0.0077 0.0321 0.0573 0.0752
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0.80 -0.0010 -0.0010 0.0251 0.0508 0.0711
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0.85 -0.0010 -0.0010 0.0175 0.0441 0.0660
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0.90 -0.0010 -0.0010 0.0110 0.0375 0.0602
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0.95 -0.0010 -0.0010 0.0027 0.0308 0.0544
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1.00 -0.0010 -0.0010 -0.0010 0.0240 0.0482
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1.05 -0.0010 -0.0010 -0.0010 0.0172 0.0420
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1.10 -0.0010 -0.0010 -0.0010 0.0106 0.0355
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1.15 -0.0010 -0.0010 -0.0010 0.0040 0.0290
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1.20 -0.0010 -0.0010 -0.0010 -0.0010 0.0222
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1.25 -0.0010 -0.0010 -0.0010 -0.0010 0.0155
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1.30 -0.0010 -0.0010 -0.0010 -0.0010 0.0085
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1.35 -0.0010 -0.0010 -0.0010 -0.0010 -0.0010
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C_POWER 25 5
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11.0 15.0 19.0 23.0 27.0
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0.10 0.0283 0.0394 0.0558 0.0822 0.1125
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0.15 0.0277 0.0400 0.0554 0.0801 0.1094
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0.20 0.0267 0.0401 0.0550 0.0785 0.1058
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0.25 0.0253 0.0398 0.0543 0.0763 0.1023
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0.30 0.0238 0.0393 0.0535 0.0741 0.0992
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0.35 0.0220 0.0387 0.0525 0.0717 0.0962
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0.40 0.0196 0.0371 0.0514 0.0698 0.0945
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0.45 0.0169 0.0351 0.0500 0.0678 0.0918
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0.50 0.0138 0.0319 0.0487 0.0668 0.0890
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0.55 0.0100 0.0272 0.0464 0.0652 0.0865
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0.60 0.0056 0.0225 0.0432 0.0637 0.0850
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0.65 0.0000 0.0179 0.0393 0.0619 0.0837
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0.70 0.0000 0.0128 0.0350 0.0590 0.0820
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0.75 0.0000 0.0077 0.0298 0.0552 0.0797
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0.80 0.0000 0.0000 0.0249 0.0512 0.0766
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0.85 0.0000 0.0000 0.0191 0.0465 0.0729
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0.90 0.0000 0.0000 0.0139 0.0414 0.0688
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0.95 0.0000 0.0000 0.0080 0.0357 0.0642
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1.00 0.0000 0.0000 0.0000 0.0299 0.0591
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1.05 0.0000 0.0000 0.0000 0.0244 0.0535
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1.10 0.0000 0.0000 0.0000 0.0185 0.0473
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1.15 0.0000 0.0000 0.0000 0.0155 0.0405
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1.20 0.0000 0.0000 0.0000 0.0000 0.0333
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1.25 0.0000 0.0000 0.0000 0.0000 0.0254
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1.30 0.0000 0.0000 0.0000 0.0000 0.0177
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</FG_PROPELLER>
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