Design of a morphing airfoil

• المؤلف الرئيسي: Tan, Hao Chong
• مؤلفون آخرون: Jorg Uwe Schluter
• التنسيق: Final Year Project
• اللغة: English
• منشور في: 2014
• الموضوعات: DRNTU::Engineering::Aeronautical engineering::Aerodynamics
• الوصول للمادة أونلاين: http://hdl.handle.net/10356/61009

This report studies the aerodynamic effects of a small single shape-morphing hump on a 2D NACA 4412 airfoil surface under a free stream of 0.7 Mach number and various cruising angle of attacks ranging from 0 degree to 4 degrees. The results are collected using Reynolds Averaged Navier Stokes Simulat...