The aerodynamic characteristics of several supercritical airfoils interim to the improved 10-percent thick NASA supercritical airfoil 26a are discussed. The airfoils have related slope and curvature distributions over the rear which result in different aft camber. For identification, the airfoils are designated supercritical airfoils 12, 13, 21, 22, and 24. Data is presented without analysis.
Aerodynamic Characteristics of 10 Percent Thick NASA Supercritical Airfoils with Different Aft Camber
1975
192 pages
Report
Keine Angabe
Englisch