Title
High Angle Of Attack Helicopter Blade-Vortex Interaction; Numerical Studies Using Les
Abstract
The influence of angle of attack on the helicopter blade-vortex mechanism of interaction is investigated using large eddy simulation (LES). The LES technique provides a promising tool for obtaining the unsteady wall-pressure fields, aerodynamic coefficients and the acoustic source functions. A large eddy simulation is carried out for a two-dimensional Blade-Vortex Interaction (BVI) problem, for a chord based Reynolds number of 1.3x106. Computations are carried out to investigate the influence of angle of attack (α = 0θ, α = 5θ, α = 10θ) on the aerodynamic coefficients and acoustic field. © 2011 by Marcel Ilie.
Publication Date
12-1-2011
Publication Title
20th AIAA Computational Fluid Dynamics Conference 2011
Number of Pages
-
Document Type
Article; Proceedings Paper
Personal Identifier
scopus
Copyright Status
Unknown
Socpus ID
84880641769 (Scopus)
Source API URL
https://api.elsevier.com/content/abstract/scopus_id/84880641769
STARS Citation
Al-Kuran, Husam; Coronado, Patricia; Ilie, Marcel; and Zha, Ge Cheng, "High Angle Of Attack Helicopter Blade-Vortex Interaction; Numerical Studies Using Les" (2011). Scopus Export 2010-2014. 2151.
https://stars.library.ucf.edu/scopus2010/2151