Dynamic inflow-based analysis of pitch changes to hovering rotor

• المؤلف الرئيسي: Banerjee, Tridib
• مؤلفون آخرون: -
• التنسيق: Thesis-Master by Coursework
• اللغة: English
• منشور في: Nanyang Technological University 2020
• الموضوعات: Engineering::Aeronautical engineering::Aerodynamics; Engineering::Aeronautical engineering::Propellers
• الوصول للمادة أونلاين: https://hdl.handle.net/10356/144208

There are two parts to solving rotor aerodynamics. First is pertaining to the rotor blades and other to the wake. Dynamic inflow modelling is a computationally cheap framework to estimate the latter. It is essentially an approach to recreate the non-uniform pressure (and by extension, inflow) distri...