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 0.06 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 0.0697 0.0808 0.0949 0.1058 0.0997
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0.15 0.0638 0.0795 0.0901 0.1012 0.1000
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0.20 0.0573 0.0773 0.0861 0.0970 0.1000
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0.25 0.0508 0.0740 0.0826 0.0936 0.0992
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0.30 0.0442 0.0697 0.0793 0.0898 0.0980
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0.35 0.0374 0.0637 0.0763 0.0866 0.0962
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0.40 0.0305 0.0574 0.0739 0.0831 0.0941
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0.45 0.0230 0.0501 0.0700 0.0803 0.0918
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0.50 0.0154 0.0425 0.0655 0.0780 0.0890
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0.55 0.0079 0.0340 0.0586 0.0764 0.0855
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0.60 -0.0010 0.0265 0.0518 0.0727 0.0820
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0.65 -0.0010 0.0188 0.0450 0.0680 0.0786
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0.70 -0.0010 0.0119 0.0380 0.0621 0.0757
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0.75 -0.0010 0.0043 0.0309 0.0556 0.0735
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0.80 -0.0010 -0.0010 0.0238 0.0488 0.0702
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0.85 -0.0010 -0.0010 0.0165 0.0422 0.0658
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0.90 -0.0010 -0.0010 0.0091 0.0357 0.0600
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0.95 -0.0010 -0.0010 0.0018 0.0287 0.0546
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1.00 -0.0010 -0.0010 -0.0010 0.0216 0.0489
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1.05 -0.0010 -0.0010 -0.0010 0.0154 0.0428
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1.10 -0.0010 -0.0010 -0.0010 0.0080 0.0356
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1.15 -0.0010 -0.0010 -0.0010 -0.0010 0.0290
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1.20 -0.0010 -0.0010 -0.0010 -0.0010 0.0218
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1.25 -0.0010 -0.0010 -0.0010 -0.0010 0.0147
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1.30 -0.0010 -0.0010 -0.0010 -0.0010 0.0080
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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 0.0269 0.0408 0.0704 0.0980 0.1132
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0.15 0.0260 0.0410 0.0652 0.0935 0.1128
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0.20 0.0249 0.0403 0.0607 0.0890 0.1123
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0.25 0.0234 0.0397 0.0560 0.0848 0.1118
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0.30 0.0215 0.0383 0.0533 0.0809 0.1100
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0.35 0.0196 0.0372 0.0514 0.0771 0.1076
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0.40 0.0172 0.0354 0.0504 0.0734 0.1049
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0.45 0.0142 0.0325 0.0493 0.0698 0.1019
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0.50 0.0109 0.0290 0.0479 0.0676 0.0981
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0.55 0.0069 0.0247 0.0446 0.0661 0.0939
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0.60 0.0000 0.0206 0.0412 0.0640 0.0891
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0.65 0.0000 0.0162 0.0377 0.0612 0.0851
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0.70 0.0000 0.0118 0.0334 0.0579 0.0818
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0.75 0.0000 0.0070 0.0289 0.0533 0.0793
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0.80 0.0000 0.0000 0.0238 0.0489 0.0764
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0.85 0.0000 0.0000 0.0181 0.0443 0.0732
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0.90 0.0000 0.0000 0.0122 0.0394 0.0684
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0.95 0.0000 0.0000 0.0060 0.0337 0.0645
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1.00 0.0000 0.0000 0.0000 0.0273 0.0600
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1.05 0.0000 0.0000 0.0000 0.0203 0.0547
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1.10 0.0000 0.0000 0.0000 0.0135 0.0477
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1.15 0.0000 0.0000 0.0000 0.0000 0.0410
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1.20 0.0000 0.0000 0.0000 0.0000 0.0326
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1.25 0.0000 0.0000 0.0000 0.0000 0.0245
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1.30 0.0000 0.0000 0.0000 0.0000 0.0160
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</FG_PROPELLER>
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