Dynamic inflow-based analysis of pitch changes to hovering rotor

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...

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Bibliographic Details
Main Author: Banerjee, Tridib
Other Authors: -
Format: Thesis-Master by Coursework
Language:English
Published: Nanyang Technological University 2020
Subjects:
Online Access:https://hdl.handle.net/10356/144208