NACA 2415 airfoilMax thickness 15% at 29.5% chordMax camber 2% at 39.6% chordSource UIUC Airfoil Coordinates Database (n6409-il) NACA6409 9% Airfoil detailsSend to airfoil plotterAdd to comparisonLednicer format dat fileSelig format dat fileSource dat file NACA 6409Max thickness 9% at 29.3%...
This introduction is followed by the results from the wind tunnel testing of a NACA 2415 wing and the analysis of this data. The analysis is to be used for the construction of a radio controlled Vertical Take Off and Land vehicle (VTOL) model, with the potential for use on a full- ...
Send to airfoil plotterAdd to comparisonAdd to My airfoils NACA 4 digit airfoils in the database NACA 0006 NACA 0008 NACA 0009 NACA 0010 NACA 0012 NACA 0015 NACA 0018 NACA 0021 NACA 0024 NACA 1408 NACA 1410 NACA 1412 NACA 2408 NACA 2410 NACA 2411 NACA 2412 NACA 2414 NACA 2415 NACA ...
Send to airfoil plotterAdd to comparisonAdd to My airfoils NACA 4 digit airfoils in the database NACA 0006 NACA 0008 NACA 0009 NACA 0010 NACA 0012 NACA 0015 NACA 0018 NACA 0021 NACA 0024 NACA 1408 NACA 1410 NACA 1412 NACA 2408 NACA 2410 NACA 2411 NACA 2412 NACA 2414 NACA 2415 NACA ...