Theoretical Prediction of Thick Wing and Pylon-Fuselage-Fanpod-Nacelle Aerodynamic Characteristics at Subcritical Speeds. Part 2: Computer Program Description

摘要

The procedures required to operate the thick wing and pylon-fuselage-fanpod-nacelle computer program are presented. The program computes surface velocities and pressure, section loads, and total configuration loads and pitching moment. Potential flow theory is used to compute the surface pressures and the associated lift, moment, and vortex drag. The skin friction drag is also computed. (Author)