Numerical Analysis of Glauert Inflow Formula for Single-Rotor Helicopter in Steady-Level Flight below Stall-Flutter Limit

This article addresses the numerical computation problem of induced inflow ratio based on the helicopter momentum theory in forward flight. The Glauert inflow formula (equation) is a nonlinear equation usually solved by the Newton–Raphson method in a relatively small number of iterations. However, m...

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Bibliographic Details
Main Authors: Marjan Dodic, Branimir Krstic, Bosko Rasuo, Mirko Dinulovic, Aleksandar Bengin
Format: Article
Language:English
Published: MDPI AG 2023-02-01
Series:Aerospace
Subjects:
Online Access:https://www.mdpi.com/2226-4310/10/3/238