A computer program developed to calculate the ordinates and surface slopes of any thickness, symmetrical or cambered NACA airfoil of the 4-digit, 4-digit modified, 5-digit, and 16-series airfoil families is presented. The program produces plots of the airfoil nondimensional ordinates and a punch card output of ordinates in the input format of a readily available program for determining the pressure distributions of arbitrary airfoils in subsonic potential viscous flow. (Author)
Development of a Computer Program to Obtain Ordinates for Naca 4-Digit, 4-Digit Modified, 5-Digit, and 16 Series Airfoils
1975
45 pages
Report
No indication
English