Naca

PDAS home > Contents > NACA aerofoil > AVD Appendices > 4- and 5- physical body Sections populace Domain aeronautic software product (PDAS)   Appendix III - 4 and 5 Digit Sections Go back to the AVD main page let the page give the outpouring loading before clicking on a section. Four number cambered sections 1408 1410 1412 2408 2410 2412 2415 2418 2421 2424 4412 4415 4418 4421 4424 Five-digit cambered sections 23012 23015 23018 23021 23024 NACA Section 1408| ( lays and ordinates given in per cent of airfoil chord)| upper ascend| Lower dismount along| complete in| hallow| rank| range| 0.0000| 0.0000| 0.0000| 0.0000| 0.5000| 0.8729| 0.5000| -0.7583| 0.7500| 1.0590| 0.7500| -0.9240| 1.2500| 1.3553| 1.2500| -1.1734| 2.5000| 1.8921| 2.5000| -1.5982| 5.0000| 2.6273| 5.0000| -2.1168| 7.5000| 3.1588| 7.5000| -2.4456| 10.0000| 3.5746| 10.0000| -2.6733| 15.0000| 4.1820| 15.0000| -2.9482| 20.0000| 4.5799| 20.0000| -3.0725| 25.0000| 4.8221| 25.0000| -3.1009| 30.0000| 4.9390| 30.0000| -3.0640| 35.0000| 4.9499| 35.0000| -2.9818| 40.0000| 4.8687| 40.0000| -2.8687| 45.0000| 4.7139| 45.0000| -2.7271| 50.0000| 4.5025| 50.0000| -2.5564| 55.0000| 4.2406| 55.0000| -2.3629| 60.0000| 3.9332| 60.0000| -2.1517| 65.

0000| 3.5839| 65.0000| -1.9266| 70.0000| 3.1956| 70.0000| -1.6903| 75.0000| 2.7698| 75.0000| -1.4447| 80.0000| 2.3076| 80.0000| -1.1908| 85.0000| 1.8090| 85.0000| -0.9286| 90.0000| 1.2733| 90.0000| -0.6577| 95.0000| 0.6991| 95.0000| -0.3768| 100.0000| 0.0843| 100.0000| -0.0838| L.E. radius = 0.705 percent c| slope of mean line at LE = 0.0500| | NACA 1408| (Stations and ordinates given in per cent of airfoil chord)| top(prenominal) Surface| Lower Surface| Station| Ordinate| Station| Ordinate| 0.0000| 0.0000| 0.0000| 0.0000| 0.4598| 0.8381| 0.5402| -0.7884| 0.7015| 1.0259| 0.7985| -0.9516...If you want to get a full essay, come out it on our website: Ordercustompaper.com

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