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DRAGONFLY CANARD (drgnfly-il)

DRAGONFLY CANARD - Dragonfly Canard airfoil


Airfoil drgnfly-il
Details Dat file Parser  
(drgnfly-il) DRAGONFLY CANARD
Dragonfly Canard airfoil
Max thickness 19.3% at 37.6% chord.
Max camber 6.6% at 40.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
DRAGONFLY CANARD
      74.0      67.0
 
 0.0000000 0.0000000
 0.0001457 0.0020791
 0.0005989 0.0043226
 0.0013409 0.0066716
 0.0023466 0.0091410
 0.0036141 0.0117609
 0.0051572 0.0145612
 0.0070160 0.0175760
 0.0092433 0.0208453
 0.0119110 0.0244164
 0.0151171 0.0283474
 0.0189834 0.0327004
 0.0236648 0.0375507
 0.0293351 0.0429706
 0.0361713 0.0490064
 0.0443123 0.0556434
 0.0538113 0.0627835
 0.0646016 0.0702568
 0.0765326 0.0778690
 0.0894156 0.0854478
 0.1030717 0.0928688
 0.1173461 0.1000490
 0.1321090 0.1069300
 0.1472595 0.1134707
 0.1627235 0.1196449
 0.1784441 0.1254346
 0.1943784 0.1308288
 0.2104903 0.1358162
 0.2267510 0.1403919
 0.2431323 0.1445470
 0.2596113 0.1482752
 0.2761710 0.1515715
 0.2927934 0.1544291
 0.3094666 0.1568438
 0.3261755 0.1588125
 0.3428982 0.1603344
 0.3596047 0.1614033
 0.3762569 0.1620161
 0.3928149 0.1621598
 0.4092597 0.1618164
 0.4256004 0.1609678
 0.4418859 0.1595972
 0.4581774 0.1577047
 0.4745027 0.1553063
 0.4908638 0.1524111
 0.5072857 0.1490139
 0.5238335 0.1451140
 0.5405811 0.1407256
 0.5575834 0.1358796
 0.5748784 0.1306111
 0.5925030 0.1249652
 0.6104801 0.1189999
 0.6287965 0.1127943
 0.6473631 0.1064491
 0.6660159 0.1000650
 0.6846015 0.0937368
 0.7030689 0.0875234
 0.7214391 0.0814578
 0.7397921 0.0755411
 0.7582108 0.0697446
 0.7767314 0.0640372
 0.7953659 0.0584011
 0.8141143 0.0528190
 0.8329656 0.0472762
 0.8518957 0.0417615
 0.8708630 0.0362789
 0.8898250 0.0308382
 0.9087250 0.0254544
 0.9274510 0.0201603
 0.9457506 0.0150235
 0.9631459 0.0101742
 0.9789165 0.0058041
 0.9923993 0.0020880
 1.0000000 0.0000000
 
 0.0000000 0.0000000
 0.0001805 -.0021814
 0.0007254 -.0043563
 0.0016289 -.0065105
 0.0028783 -.0086312
 0.0044806 -.0106863
 0.0064676 -.0126248
 0.0088683 -.0143915
 0.0117057 -.0159566
 0.0150096 -.0173100
 0.0188391 -.0184784
 0.0232904 -.0195358
 0.0285087 -.0206030
 0.0346850 -.0217715
 0.0420663 -.0230410
 0.0509365 -.0243420
 0.0616005 -.0256040
 0.0743312 -.0267916
 0.0891285 -.0279337
 0.1055755 -.0289830
 0.1231631 -.0298795
 0.1414954 -.0306087
 0.1603064 -.0311991
 0.1794002 -.0316631
 0.1986707 -.0320168
 0.2180541 -.0322683
 0.2375143 -.0324307
 0.2570233 -.0325080
 0.2765712 -.0325062
 0.2961400 -.0324295
 0.3157297 -.0322787
 0.3353333 -.0320599
 0.3549327 -.0317761
 0.3744961 -.0314273
 0.3939943 -.0309987
 0.4134563 -.0304722
 0.4329322 -.0298456
 0.4524549 -.0291260
 0.4720535 -.0283253
 0.4917410 -.0274584
 0.5115053 -.0265464
 0.5313196 -.0256013
 0.5511649 -.0246262
 0.5710391 -.0236260
 0.5909453 -.0226027
 0.6108834 -.0215655
 0.6308455 -.0205211
 0.6508187 -.0194718
 0.6707878 -.0184254
 0.6907469 -.0173861
 0.7106941 -.0163568
 0.7306303 -.0153385
 0.7505585 -.0143333
 0.7704768 -.0133430
 0.7903870 -.0123678
 0.8102773 -.0114096
 0.8301386 -.0104724
 0.8499590 -.0095623
 0.8697084 -.0086753
 0.8892588 -.0077757
 0.9084961 -.0068145
 0.9273193 -.0057571
 0.9455405 -.0045867
 0.9628015 -.0033160
 0.9785467 -.0020097
 0.9921971 -.0007620
 1.0000000 0.0000000
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Polars for DRAGONFLY CANARD (drgnfly-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   drgnfly-il50,00093.9 at α=12.5°Mach=0 Ncrit=9Xfoil predictionDetails
   drgnfly-il50,00055.8 at α=14.5°Mach=0 Ncrit=5Xfoil predictionDetails
   drgnfly-il100,00094.7 at α=13.25°Mach=0 Ncrit=9Xfoil predictionDetails
   drgnfly-il100,00058.4 at α=9.75°Mach=0 Ncrit=5Xfoil predictionDetails
   drgnfly-il200,00098.8 at α=13.25°Mach=0 Ncrit=9Xfoil predictionDetails
   drgnfly-il200,000545.8 at α=2.25°Mach=0 Ncrit=5Xfoil predictionDetails
   drgnfly-il500,000987.8 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   drgnfly-il500,0005104.7 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   drgnfly-il1,000,0009144.6 at α=9.25°Mach=0 Ncrit=9Xfoil predictionDetails
   drgnfly-il1,000,0005149.1 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
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