DU 86-137/25 DB Name: du861372 Family: Delft Max thickness: 13.7% at x = 39.72% chord Max camber: 0.2% at x = 9.71% chord Available data sources: JavaFoil+Calcfoil stall+Eppler ext transition XFOIL ncrit=9
Notes:
Coordinates and information in these papers:
Boermans & Bennis, "DESIGN AND WINDTUNNEL TESTS OF AN AIRFOIL FOR THE HORIZONTAL TAILPLANE OF A STANDARD CLASS SAILPLANE,"
Technical Soaring, Vol 16 No 2 (1992).
Boermans & Bennis, "Errata for 'DESIGN AND WIND TUNNEL TESTS OF AN AIRFOIL FOR THE HORIZONTAL TAILPLANE OF A STANDARD CLASS GLIDER'," Technical Soaring, Vol 17 No 1 (1993).
Boermans & Bennis, "Addition to 'Design and wind tunnel tests of an airfoil for the horizontal tailplane of a Standard Class glider'," Technical Soaring, Vol 17 No 3 (1993).