PSU 94-097 (AIAA 2001-2478) (psu94097-il)
PSU 94-097 (AIAA 2001-2478) - Maughmer PSU 94-097 winglet airfoil
| Details | Dat file | Parser | |
|
(psu94097-il) PSU 94-097 (AIAA 2001-2478) Maughmer PSU 94-097 winglet airfoil Max thickness 9.7% at 32.3% chord. Max camber 4% at 46.3% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
PSU 94-097 (AIAA 2001-2478) 1.00000 0.00328 0.99709 0.00385 0.98838 0.00554 0.97398 0.00834 0.95406 0.01223 0.92886 0.01720 0.89868 0.02324 0.86517 0.03004 0.82800 0.03739 0.78772 0.04510 0.74490 0.05297 0.70009 0.06072 0.65387 0.06808 0.60678 0.074687 0.55916 0.080114 0.51121 0.084172 0.46324 0.086875 0.41564 0.088198 0.36876 0.088194 0.32305 0.086965 0.27899 0.084563 0.23701 0.081085 0.19757 0.076557 0.16104 0.071033 0.12778 0.064574 0.09803 0.057235 0.07200 0.049133 0.04983 0.040464 0.03163 0.031443 0.01749 0.022374 0.00747 0.013622 0.00164 0.005664 0.00008 0.00099 0.00002 -0.0004 0.00031 -0.0016 0.00109 -0.0026 0.00237 -0.0036 0.00450 -0.0048 0.01504 -0.0084 0.03099 -0.0113 0.05223 -0.0134 0.07861 -0.0147 0.10991 -0.0152 0.14580 -0.0151 0.18595 -0.0144 0.22994 -0.0132 0.27724 -0.0117 0.32729 -0.0099 0.37951 -0.0080 0.43325 -0.0060 0.48785 -0.0039 0.54273 -0.0017 0.59735 0.00039 0.65110 0.00238 0.70331 0.00407 0.75332 0.00535 0.80042 0.00612 0.84394 0.00635 0.88321 0.00603 0.91760 0.00522 0.94656 0.00405 0.96959 0.00270 0.98635 0.00141 0.99656 0.00041 1.00000 0.00000 |
No parser warnings |
Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file |
Similar airfoils
|
Polars for PSU 94-097 (AIAA 2001-2478) (psu94097-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| psu94097-il | 50,000 | 9 | 39.2 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| psu94097-il | 50,000 | 5 | 41.2 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| psu94097-il | 100,000 | 9 | 64 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| psu94097-il | 100,000 | 5 | 64.1 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| psu94097-il | 200,000 | 9 | 90.8 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| psu94097-il | 200,000 | 5 | 86.8 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| psu94097-il | 500,000 | 9 | 126.6 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| psu94097-il | 500,000 | 5 | 112.9 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| psu94097-il | 1,000,000 | 9 | 150.7 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| psu94097-il | 1,000,000 | 5 | 127.5 at α=2.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| Reynolds number calculator | |||||||