Impact of optimized variable rotor speed and active blade twist control on helicopter blade–vortex interaction noise and environmental impact

51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition ◽

Aerodynamic aspects of helicopter blade-vortex interaction; the interaction with vortex streets considering the icing effect

10.2514/6.2013-243 ◽

2013 ◽

Author(s):

Marcel Ilie

Keyword(s):

Vortex Interaction ◽

Helicopter Blade ◽

Vortex Streets

Analysis of Helicopter Blade-Vortex Interaction Noise with Flight Path or Attitude Modification

10.4050/1.3092850 ◽

2005 ◽

Vol 50 (2) ◽

pp. 123-137 ◽

Cited By ~ 2

Author(s):

Brian Munsky ◽

Farhan Gandhi

Keyword(s):

Flight Path ◽

Vortex Interaction ◽

Helicopter Blade ◽

Attitude Modification

Active control of blade vortex interaction noise on a helicopter blade element

10.1117/12.316333 ◽

1998 ◽

Author(s):

Kartik B. Ariyur ◽

Miroslav Krstic

Keyword(s):

Active Control ◽

Vortex Interaction ◽

Helicopter Blade ◽

Blade Element

49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition ◽

High angle of attack helicopter blade-vortex interaction; numerical studies using LES

10.2514/6.2011-55 ◽

2011 ◽

Author(s):

Marcel Ilie ◽

Patricia Coronado ◽

Carlos Velez ◽

Ge-Cheng Zha

Keyword(s):

Angle Of Attack ◽

Vortex Interaction ◽

High Angle ◽

High Angle Of Attack ◽

Helicopter Blade ◽

Numerical Studies ◽

Critical Aerodynamic Aspects of Helicopter Blade-Vortex Interaction: A Numerical Study Using Large-Eddy Simulation

27th AIAA Applied Aerodynamics Conference ◽

10.2514/6.2009-3858 ◽

2009 ◽

Cited By ~ 1

Author(s):

Marcel Ilie ◽

Stephan Llewellyn Smith

Keyword(s):

Large Eddy Simulation ◽

Numerical Study ◽

Vortex Interaction ◽

Helicopter Blade ◽

Eddy Simulation ◽

Large Eddy

Quasi-Static Flight Path Control of Helicopter Blade Vortex Interaction Noise in a Steady Wind

10.4050/jahs.52.15 ◽

2007 ◽

Vol 52 (1) ◽

pp. 15-23 ◽

Cited By ~ 1

Author(s):

Gaurav Gopalan ◽

Fredric H. Schmitz

Keyword(s):

Flight Path ◽

Vortex Interaction ◽

Helicopter Blade ◽

Path Control ◽

Effect of Leading-Edge Serrations on Helicopter Blade–Vortex Interaction Noise

10.4050/jahs.62.032001 ◽

2017 ◽

Vol 62 (3) ◽

pp. 1-11 ◽

Cited By ~ 2

Author(s):

Joel A. Feinerman ◽

Sudarshan Koushik ◽

Fredric H. Schmitz

Keyword(s):

Leading Edge ◽

Vortex Interaction ◽

Helicopter Blade ◽

Reduction of helicopter blade-vortex interaction noise by active rotor control technology

Progress in Aerospace Sciences ◽

10.1016/s0376-0421(97)00006-7 ◽

1997 ◽

Vol 33 (9-10) ◽

pp. 647-687 ◽

Cited By ~ 21

Author(s):

Yung H. Yu ◽

Bernd Gmelin ◽

Wolf Splettstoesser ◽

Jean J. Philippe ◽

Jean Prieur ◽

...

Keyword(s):

Control Technology ◽

Vortex Interaction ◽

Helicopter Blade ◽

Active Rotor Control ◽

Rotor Control

Feedback attenuation and adaptive cancellation of blade vortex interaction on a helicopter blade element

IEEE Transactions on Control Systems Technology ◽

10.1109/87.784423 ◽

1999 ◽

Vol 7 (5) ◽

pp. 596-605 ◽

Cited By ~ 35

Author(s):

K.B. Ariyur ◽

M. Krstic

Keyword(s):

Vortex Interaction ◽

Helicopter Blade ◽

Adaptive Cancellation ◽

Blade Element

Radiation and Directionality Characteristics of Helicopter Blade-Vortex Interaction Noise

10.4050/jahs.48.253 ◽

2003 ◽

Vol 48 (4) ◽

pp. 253-269 ◽

Cited By ~ 10

Author(s):

Fredric H. Schmitz ◽

Ben Wel-C. Sim

Keyword(s):

Vortex Interaction ◽

Helicopter Blade ◽