NASA LRN 1015 (NASA TM 102840) (lrn1015-il)
NASA LRN 1015 (NASA TM 102840) - LRN 1015 airfoil used on the Northrop Grumman RQ-4 Global Hawk airfoil
| Details | Dat file | Parser | |
|
(lrn1015-il) NASA LRN 1015 (NASA TM 102840) LRN 1015 airfoil used on the Northrop Grumman RQ-4 Global Hawk airfoil Max thickness 15.2% at 40% chord. Max camber 4.9% at 44% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
NASA LRN 1015 (NASA TM 102840) 1.000000 0.000000 0.998379 0.000577 0.993525 0.002244 0.985471 0.004834 0.974268 0.008107 0.959990 0.011820 0.942728 0.015794 0.922595 0.020019 0.899721 0.024801 0.874255 0.030724 0.846362 0.037889 0.816223 0.046102 0.784032 0.055549 0.750000 0.066230 0.714346 0.077492 0.677302 0.088455 0.639109 0.098407 0.600013 0.106947 0.560268 0.113813 0.520133 0.118919 0.479867 0.122351 0.439732 0.124264 0.399987 0.124809 0.360891 0.124114 0.322698 0.122299 0.285654 0.119458 0.250000 0.115663 0.215968 0.110974 0.183777 0.105433 0.153638 0.099088 0.125745 0.092004 0.100279 0.084202 0.077405 0.075746 0.057272 0.066677 0.040010 0.057142 0.025732 0.046990 0.014529 0.036312 0.006475 0.026197 0.001621 0.017070 0.000000 0.000000 0.001621 -0.001976 0.006475 -0.004930 0.014529 -0.007513 0.025732 -0.010010 0.040010 -0.012525 0.057272 -0.014983 0.077405 -0.017226 0.100279 -0.019318 0.125745 -0.021214 0.153638 -0.022877 0.183777 -0.024304 0.215968 -0.025466 0.250000 -0.026357 0.285654 -0.026977 0.322698 -0.027302 0.360891 -0.027330 0.399987 -0.027065 0.439732 -0.026505 0.479867 -0.025652 0.520133 -0.024494 0.560268 -0.023028 0.600013 -0.021274 0.639109 -0.019239 0.677302 -0.016865 0.714346 -0.014081 0.750000 -0.010938 0.784032 -0.007663 0.816223 -0.004646 0.846362 -0.002130 0.874255 -0.000215 0.899721 0.001069 0.922595 0.001761 0.942728 0.001957 0.959990 0.001792 0.974268 0.001378 0.985471 0.000884 0.993525 0.000429 0.998379 0.000113 1.000000 0.000000 |
No parser warnings |
Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file |
Similar airfoils
|
Polars for NASA LRN 1015 (NASA TM 102840) (lrn1015-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| lrn1015-il | 50,000 | 9 | 21.9 at α=12.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| lrn1015-il | 50,000 | 5 | 20.2 at α=11° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| lrn1015-il | 100,000 | 9 | 39.8 at α=9.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| lrn1015-il | 100,000 | 5 | 34 at α=9° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| lrn1015-il | 200,000 | 9 | 70.8 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| lrn1015-il | 200,000 | 5 | 72.6 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| lrn1015-il | 500,000 | 9 | 127.7 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| lrn1015-il | 500,000 | 5 | 112.9 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| lrn1015-il | 1,000,000 | 9 | 154.8 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| lrn1015-il | 1,000,000 | 5 | 134.4 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| Reynolds number calculator | |||||||