3390000b98
two-blade aluminum prop (provided to Jon by Hartzell) + 10% for the engine (at Jon's suggestion).
68 lines
2.8 KiB
XML
68 lines
2.8 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 27 5
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11.0 15.0 19.0 23.0 27.0
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0.10 0.0750 0.0818 0.0910 0.0870 0.0950
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0.15 0.0670 0.0795 0.0910 0.0882 0.0933
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0.20 0.0630 0.0770 0.0900 0.0889 0.0925
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0.25 0.0580 0.0742 0.0884 0.0890 0.0915
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0.30 0.0525 0.0702 0.0860 0.0890 0.0908
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0.35 0.0460 0.0660 0.0832 0.0886 0.0898
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0.40 0.0395 0.0612 0.0801 0.0880 0.0888
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0.45 0.0330 0.0560 0.0757 0.0864 0.0882
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0.50 0.0255 0.0500 0.0708 0.0845 0.0880
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0.55 0.0170 0.0416 0.0655 0.0817 0.0877
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0.60 0.0095 0.0330 0.0591 0.0780 0.0870
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0.65 -0.0010 0.0248 0.0520 0.0732 0.0858
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0.70 -0.0010 0.0175 0.0450 0.0672 0.0830
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0.75 -0.0010 0.0105 0.0368 0.0610 0.0800
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0.80 -0.0010 -0.0010 0.0294 0.0547 0.0752
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0.85 -0.0010 -0.0010 0.0224 0.0483 0.0703
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0.90 -0.0010 -0.0010 -0.0010 0.0416 0.0651
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0.95 -0.0010 -0.0010 -0.0010 0.0349 0.0591
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1.00 -0.0010 -0.0010 -0.0010 0.0280 0.0530
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1.05 -0.0010 -0.0010 -0.0010 0.0211 0.0467
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1.10 -0.0010 -0.0010 -0.0010 0.0142 0.0402
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1.15 -0.0010 -0.0010 -0.0010 0.0072 0.0337
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1.20 -0.0010 -0.0010 -0.0010 -0.0010 0.0270
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1.25 -0.0010 -0.0010 -0.0010 -0.0010 0.0201
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1.30 -0.0010 -0.0010 -0.0010 -0.0010 0.0130
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1.35 -0.0010 -0.0010 -0.0010 -0.0010 0.0056
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1.40 -0.0010 -0.0010 -0.0010 -0.0010 -0.0010
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C_POWER 26 5
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11.0 15.0 19.0 23.0 27.0
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0.10 0.0295 0.0400 0.0520 0.0769 0.1055
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0.15 0.0290 0.0400 0.0521 0.0755 0.1029
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0.20 0.0285 0.0400 0.0523 0.0740 0.1000
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0.25 0.0280 0.0400 0.0525 0.0720 0.0972
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0.30 0.0265 0.0397 0.0526 0.0695 0.0950
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0.35 0.0248 0.0392 0.0527 0.0676 0.0922
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0.40 0.0226 0.0384 0.0528 0.0663 0.0900
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0.45 0.0205 0.0370 0.0523 0.0656 0.0880
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0.50 0.0170 0.0348 0.0513 0.0658 0.0863
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0.55 0.0129 0.0302 0.0498 0.0659 0.0852
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0.60 0.0085 0.0255 0.0472 0.0656 0.0839
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0.65 0.0000 0.0208 0.0436 0.0646 0.0835
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0.70 0.0000 0.0164 0.0394 0.0620 0.0822
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0.75 0.0000 0.0115 0.0345 0.0588 0.0814
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0.80 0.0000 0.0000 0.0294 0.0551 0.0791
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0.85 0.0000 0.0000 0.0238 0.0510 0.0766
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0.90 0.0000 0.0000 0.0000 0.0461 0.0739
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0.95 0.0000 0.0000 0.0000 0.0408 0.0700
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1.00 0.0000 0.0000 0.0000 0.0349 0.0652
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1.05 0.0000 0.0000 0.0000 0.0284 0.0597
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1.10 0.0000 0.0000 0.0000 0.0214 0.0536
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1.15 0.0000 0.0000 0.0000 0.0140 0.0469
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1.20 0.0000 0.0000 0.0000 0.0000 0.0398
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1.25 0.0000 0.0000 0.0000 0.0000 0.0321
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1.30 0.0000 0.0000 0.0000 0.0000 0.0240
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1.35 0.0000 0.0000 0.0000 0.0000 0.0157
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</FG_PROPELLER>
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