Airfoil Tools
Search 1636 airfoils Google+
You have 0 airfoils loaded.
Your Reynold number range is 50,000 to 1,000,000. (set)

NLR-1T AIRFOIL (nlr1t-il)

NLR-1T AIRFOIL - Bell/NASA/NLR NLR-1T rotorcraft airfoil


Airfoil nlr1t-il
Details Dat file Parser  
(nlr1t-il) NLR-1T AIRFOIL
Bell/NASA/NLR NLR-1T rotorcraft airfoil
Max thickness 8.7% at 38.3% chord.
Max camber 1.3% at 22.3% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
 NLR-1T AIRFOIL
       33.       33.
 
 0.0       0.0
 0.00259   0.00704
 0.00974   0.01524
 0.02185   0.02296
 0.03796   0.02972
 0.05675   0.03588
 0.07753   0.04098
 0.09845   0.04469
 0.12341   0.04741
 0.15412   0.04986
 0.18767   0.05188
 0.22313   0.05345
 0.26054   0.05459
 0.29979   0.05531
 0.34064   0.05565
 0.38269   0.05560
 0.42528   0.05518
 0.46849   0.05438
 0.51162   0.05323
 0.55383   0.05175
 0.59596   0.04992
 0.63728   0.04774
 0.67732   0.04524
 0.71079   0.04291
 0.73905   0.04017
 0.76946   0.03644
 0.80263   0.03140
 0.84055   0.02533
 0.87846   0.01901
 0.90845   0.01421
 0.93589   0.01020
 0.96199   0.00651
 1.00000   0.00104
 
 0.0       0.0
 0.00259  -0.00512
 0.00974  -0.00867
 0.02185  -0.01180
 0.03796  -0.01465
 0.05675  -0.01713
 0.07753  -0.01929
 0.09845  -0.02112
 0.12341  -0.02299
 0.15412  -0.02494
 0.18767  -0.02671
 0.22313  -0.02821
 0.26054  -0.02944
 0.29979  -0.03040
 0.34064  -0.03104
 0.38269  -0.03142
 0.42528  -0.03150
 0.46849  -0.03132
 0.51162  -0.03080
 0.55383  -0.02992
 0.59596  -0.02867
 0.63728  -0.02734
 0.67732  -0.02580
 0.71079  -0.02432
 0.73905  -0.02305
 0.76946  -0.02164
 0.80263  -0.01996
 0.84055  -0.01794
 0.87846  -0.01571
 0.90845  -0.01364
 0.93589  -0.01087
 0.96199  -0.00711
 1.00000  -0.00104
No parser warnings Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file

Similar airfoils

NLR-7223-62 AIRFOILPreviewDetails
GIII BL288 AIRFOILPreviewDetails
GIII BL332 AIRFOILPreviewDetails
SIKORSKY SSC-A09 AIRFOILPreviewDetails
GIII BL369 AIRFOILPreviewDetails
GIII BL387 AIRFOILPreviewDetails
NASA/LANGLEY RC-08(N)1 AIRFOILPreviewDetails
GIII BL430 AIRFOILPreviewDetails
BOEING-VERTOL VR-15 AIRFOILPreviewDetails
GIII BL207 AIRFOILPreviewDetails

Polars for NLR-1T AIRFOIL (nlr1t-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   nlr1t-il50,000929.6 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   nlr1t-il50,000528.3 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   nlr1t-il100,000938.9 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   nlr1t-il100,000539.5 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   nlr1t-il200,000953.4 at α=2.75°Mach=0 Ncrit=9Xfoil predictionDetails
   nlr1t-il200,000552 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   nlr1t-il500,000970.5 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   nlr1t-il500,000568.2 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   nlr1t-il1,000,000984.8 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   nlr1t-il1,000,000580.9 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
Reynolds number calculator
Set Reynolds number and Ncrit rangeLowHigh
Reynolds Number
NCrit