Unsteady Aerodynamic Modeling and Analysis of Load Distribution for Helicopter Rotor Blades

2022 ◽  
Vol 35 (1) ◽  
pp. 04021106
Author(s):  
Abdallah Dayhoum ◽  
Mohamed Y. Zakaria ◽  
Omar E. Abdelhamid
Keyword(s):  
Load Distribution ◽  
Rotor Blades ◽  
Helicopter Rotor ◽  
Modeling And Analysis ◽  
Aerodynamic Modeling ◽  
Unsteady Aerodynamic ◽  
Helicopter Rotor Blades

Circulation Control Span-Wise Blowing Location Optimization for a Helicopter Rotor Blade

2010 ◽  
Author(s):  
Alan M. Didion ◽  
Jonathan Kweder ◽  
Mary Ann Clarke ◽  
James E. Smith
Keyword(s):  
Stress Reduction ◽  
Rotor Blades ◽  
Helicopter Rotor ◽  
Base Line ◽  
Control Technology ◽  
Circulation Control ◽  
High Lift ◽  
Location Optimization ◽  
Helicopter Rotor Blades ◽  
Length Reduction

Circulation control technology has proven itself useful in the area of short take-off and landing (STOL) fixed wing aircraft by decreasing landing and takeoff distances, increasing maneuverability and lift at lower speeds. The application of circulation control technology to vertical take-off and landing (VTOL) rotorcraft could also prove quite beneficial. Successful adaptation to helicopter rotor blades is currently believed to yield benefits such as increased lift, increased payload capacity, increased maneuverability, reduction in rotor diameter and a reduction in noise. Above all, the addition of circulation control to rotorcraft as controlled by an on-board computer could provide the helicopter with pitch control as well as compensate for asymmetrical lift profiles from forward flight without need for a swashplate. There are an infinite number of blowing slot configurations, each with separate benefits and drawbacks. This study has identified three specific types of these configurations. The high lift configuration would be beneficial in instances where such power is needed for crew and cargo, little stress reduction is offered over the base line configuration. The stress reduction configuration on the other hand, however, offers little extra lift but much in the way of increased rotor lifespan and shorter rotor length. Finally, the middle balanced configuration offers a middle ground between the two extremes. With this configuration, the helicopter benefits in all categories of lift, stress reduction and blade length reduction.

Linear Flap‐Lag Dynamics of Hingeless Helicopter Rotor Blades in Hover

1972 ◽  
Vol 17 (2) ◽  
pp. 2-14 ◽  
Author(s):  
Robert A. Ormiston ◽  
Dewey H. Hodges
Keyword(s):  
Rotor Blades ◽  
Helicopter Rotor ◽  
Helicopter Rotor Blades
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