Aerodynamic prediction of helicopter rotor in forward flight using blade element theory
In this study, the helicopter blade in forward-flight condition was investigated. The blade element theory (BET) was used throughout this analysis to investigate the angle of attack variations at the blade cross sections, lift distribution along the blade and effects of increasing helicopter speed....
Main Authors: | Yaakub, F., Wahab, A., Abdullah, A., Nik Mohd., N. A. R., Shamsuddin, S. S. |
---|---|
Format: | Article |
Language: | English |
Published: |
Universiti Malaysia Pahang
2017
|
Subjects: | |
Online Access: | http://eprints.utm.my/76495/1/NARNikMohd2017_AerodynamicPredictionofHelicopterRotor.pdf |
Similar Items
-
Aerodynamic prediction of helicopter rotor in forward flight using blade element theory
by: M.F. Yaakub, et al.
Published: (2017-06-01) -
Computational aerodynamics of hovering helicopter rotors
by: Nik Mohd., Nik Ahmad Ridhwan, et al.
Published: (2012) -
The Application of Combined Momentum – Blade Element Theory for Aerodynamics Analysis Helicopter Rotor Blade in the Forward Flight
by: Ghazirah, Ghazirah, et al.
Published: (2006) -
Feasibility study on improving of 5-seater helicopter forward flight speed
by: Nik Mohd., Nik Ahmad Ridhwan
Published: (2006) -
Computational fluid dynamics of unsteady aerodynamic wake on helicopter main rotor-hub assembly
by: Othman, Nurain
Published: (2022)