Experimental Study of the Three Dimensionality of Orthogonal Blade-Vortex Interaction

AIAA Journal ◽  
2002 ◽  
Vol 40 (10) ◽  
pp. 2037-2046 ◽  
Author(s):  
Tongguang Wang ◽  
C. J. Doolan ◽  
F. N. Coton ◽  
R. A. M. Galbraith
Keyword(s):  
Experimental Study ◽  
Vortex Interaction ◽  
Blade Vortex Interaction

scholarly journals Experimental Study of Active Techniques for Blade/Vortex Interaction Noise Reduction

2009 ◽  
Vol 52 (177) ◽  
pp. 159-167 ◽  
Author(s):  
Noboru KOBIKI ◽  
Atsushi MURASHIGE ◽  
Akihiko TSUCHIHASHI ◽  
Eiichi YAMAKAWA
Keyword(s):  
Experimental Study ◽  
Noise Reduction ◽  
Vortex Interaction ◽  
Blade Vortex Interaction

Experimental study of the three dimensionality of orthogonal blade-vortex interaction

AIAA Journal ◽  
2002 ◽  
Vol 40 ◽  
pp. 2037-2046
Author(s):  
T. Wang ◽  
C. J. Doolan ◽  
F. N. Coton ◽  
R. A. M. Galbraith
Keyword(s):  
Experimental Study ◽  
Vortex Interaction ◽  
Blade Vortex Interaction

Novel method for calculating two-dimensional blade vortex interaction

AIAA Journal ◽  
1997 ◽  
Vol 35 ◽  
pp. 909-912
Author(s):  
Ronald J. Epstein ◽  
John A. Rule ◽  
Donald B. Bliss
Keyword(s):  
Two Dimensional ◽  
Vortex Interaction ◽  
Blade Vortex Interaction ◽  
Novel Method

Blade-vortex interaction experiments - Velocity and vorticity fields

1990 ◽  
Author(s):  
MICHAEL WILDER ◽  
MATTHEW PESCE ◽  
DEMETRI TELIONIS ◽  
DAVIDR. POLING
Keyword(s):  
Vortex Interaction ◽  
Blade Vortex Interaction

A modified near wake dynamic model for rotor analysis

1999 ◽  
Vol 103 (1021) ◽  
pp. 143-146 ◽  
Author(s):  
T. Wang ◽  
F. N. Coton
Keyword(s):  
High Resolution ◽  
Dynamic Model ◽  
Numerical Evaluation ◽  
Helicopter Rotor ◽  
Vortex Interaction ◽  
Near Wake ◽  
Blade Vortex Interaction ◽  
Wake Model ◽  
Induced Velocity

Abstract The Beddoes near wake model, developed for high resolution blade vortex interaction computations, enables efficient numerical evaluation of the downwash due to trailed vorticity in the near wake of a helicopter rotor. The model is, however, limited by the assumption that the near wake lies in the plane of the rotor and, in some cases, by its inability to accurately evaluate the induced velocity contribution from vorticity trailed from inboard blade sections. In this paper, modifications to the method are proposed which address these issues and allow it to be used with confidence over a wider range of rotor flows.

A 3D analytical model for orthogonal blade-vortex interaction noise

2017 ◽  
Vol 399 ◽  
pp. 104-123 ◽  
Author(s):  
Michael E. Quaglia ◽  
Thomas Léonard ◽  
Stéphane Moreau ◽  
Michel Roger
Keyword(s):  
Analytical Model ◽  
Vortex Interaction ◽  
Blade Vortex Interaction
Sign in / Sign up

Export Citation Format

Share Document