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JN-153 AIRFOIL (jn153-il)

JN-153 AIRFOIL - Narramore JN153 airfoil


Airfoil jn153-il
Details Dat file Parser  
(jn153-il) JN-153 AIRFOIL
Narramore JN153 airfoil
Max thickness 17.6% at 28.2% chord.
Max camber 8.4% at 38.1% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
 JN-153 AIRFOIL
      66.0      55.0
 
 0.0000000 0.0000000
 0.0023478 0.0140157
 0.0048772 0.0210059
 0.0082966 0.0283462
 0.0126160 0.0359566
 0.0178253 0.0437770
 0.0239147 0.0517375
 0.0308640 0.0597981
 0.0386633 0.0678788
 0.0473026 0.0759595
 0.0567520 0.0839603
 0.0670013 0.0918412
 0.0780207 0.0995421
 0.0897900 0.1070132
 0.1023195 0.1141842
 0.1156189 0.1210354
 0.1296683 0.1275665
 0.1444078 0.1337778
 0.1598074 0.1396091
 0.1758069 0.1450405
 0.1923665 0.1500419
 0.2094461 0.1545733
 0.2269858 0.1585748
 0.2449555 0.1620163
 0.2633153 0.1648079
 0.2821152 0.1669495
 0.3012951 0.1684411
 0.3207950 0.1692927
 0.3405550 0.1694744
 0.3605051 0.1689361
 0.3805552 0.1675978
 0.4006254 0.1653795
 0.4205357 0.1618912
 0.4410162 0.1565829
 0.4621668 0.1501547
 0.4856274 0.1432666
 0.5092680 0.1360686
 0.5335387 0.1287307
 0.5582593 0.1213228
 0.5832899 0.1139449
 0.6084706 0.1066470
 0.6336913 0.0994591
 0.6588019 0.0924412
 0.6837024 0.0856033
 0.7082430 0.0789754
 0.7323436 0.0725774
 0.7558842 0.0664294
 0.7787746 0.0605414
 0.8008952 0.0549132
 0.8221756 0.0495550
 0.8425361 0.0444767
 0.8618765 0.0396684
 0.8801369 0.0351299
 0.8972373 0.0308713
 0.9131376 0.0268627
 0.9277580 0.0231239
 0.9410683 0.0196250
 0.9530086 0.0163660
 0.9635389 0.0133169
 0.9726491 0.0104177
 0.9804294 0.0076184
 0.9870196 0.0050289
 0.9924098 0.0028394
 0.9964999 0.0012297
 0.9991000 0.0002899
 1.0000000 0.0000000
 
 0.0000000 0.0000000
 0.0002448 -.0039587
 0.0014097 -.0085644
 0.0037100 -.0118342
 0.0077802 -.0139739
 0.0138803 -.0155934
 0.0217205 -.0168227
 0.0311905 -.0177319
 0.0422306 -.0183310
 0.0547706 -.0186599
 0.0687607 -.0187488
 0.0841207 -.0186075
 0.1008206 -.0182660
 0.1187706 -.0177345
 0.1379206 -.0170229
 0.1581905 -.0161412
 0.1795105 -.0151094
 0.2018104 -.0139275
 0.2250103 -.0125855
 0.2490302 -.0110935
 0.2737901 -.0093814
 0.2992899 -.0073792
 0.3256098 -.0051770
 0.3526796 -.0028747
 0.3803894 -.0005424
 0.4086592 0.0017600
 0.4373591 0.0040024
 0.4664090 0.0061549
 0.4956888 0.0081774
 0.5250887 0.0100399
 0.5545086 0.0117423
 0.5838385 0.0132448
 0.6129584 0.0145373
 0.6417583 0.0156197
 0.6701383 0.0164721
 0.6979983 0.0170845
 0.7252083 0.0174668
 0.7516882 0.0175990
 0.7773083 0.0175112
 0.8019983 0.0171833
 0.8256284 0.0166453
 0.8481285 0.0158872
 0.8693987 0.0149390
 0.8893387 0.0138207
 0.9078789 0.0125422
 0.9249290 0.0111337
 0.9404091 0.0096150
 0.9542593 0.0080361
 0.9663894 0.0064072
 0.9767196 0.0047680
 0.9851497 0.0032387
 0.9916798 0.0019193
 0.9963199 0.0008897
 0.9990800 0.0002299
 1.0000000 0.0000000
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Lednicer format dat file
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Polars for JN-153 AIRFOIL (jn153-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   jn153-il50,00094.6 at α=9.5°Mach=0 Ncrit=9Xfoil predictionDetails
   jn153-il50,00056.5 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   jn153-il100,00095.6 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   jn153-il100,000518.1 at α=1.25°Mach=0 Ncrit=5Xfoil predictionDetails
   jn153-il200,000916.6 at α=1.25°Mach=0 Ncrit=9Xfoil predictionDetails
   jn153-il200,000544.6 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   jn153-il500,000998.8 at α=11.5°Mach=0 Ncrit=9Xfoil predictionDetails
   jn153-il500,0005112.6 at α=10.75°Mach=0 Ncrit=5Xfoil predictionDetails
   jn153-il1,000,0009163.3 at α=11°Mach=0 Ncrit=9Xfoil predictionDetails
   jn153-il1,000,0005165.9 at α=9°Mach=0 Ncrit=5Xfoil predictionDetails
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