Numerical investigation on influence of fuselage on multirotor wake vortex structures in forward flight

• المؤلفون الرئيسيون: Wang, John Chung-Hung, Nathanael, Joshua Christian, Low, Kin Huat
• مؤلفون آخرون: School of Mechanical and Aerospace Engineering
• التنسيق: Conference or Workshop Item
• اللغة: English
• منشور في: 2022
• الموضوعات: Engineering::Aeronautical engineering::Aircraft motors and engines; Unmanned Aerial System; Aircraft Stabilizer
• الوصول للمادة أونلاين: https://hdl.handle.net/10356/155580
• المؤسسة: Nanyang Technological University

With the increase interest in utilizing multirotorUAS in very lowaltitude airspace, the safety aspect associated with higher UAS density gains importance. One of the safety consideration is the separation requirements for UAS sharing the airspace, which consists of two major components: wake-base...