An experimental investigation on tapered wings with leading-edge protuberances

• المؤلف الرئيسي: Ee, Marcus Joon Leng
• مؤلفون آخرون: New Tze How, Daniel
• التنسيق: Final Year Project
• اللغة: English
• منشور في: Nanyang Technological University 2023
• الموضوعات: Engineering::Aeronautical engineering::Aerodynamics; Engineering::Aeronautical engineering::Aircraft
• الوصول للمادة أونلاين: https://hdl.handle.net/10356/168370
• المؤسسة: Nanyang Technological University

Particle Image Velocimetry (PIV) experiments were conducted in a water tunnel to study vortex interactions around tapered swept wings with leading edge tubercles. Two airfoil models based on the SD7032 airfoil profile were tested at Reynolds number 9100 and angles of attack (α) of -10°,10° and 25°,...