Active flow control using pulsed micro-jets on a full-scale production car

2014 ◽  
Vol 6 (1) ◽  
pp. 1-20 ◽  
Author(s):  
Jean-Luc Aider ◽  
Pierric Joseph ◽  
Tony Ruiz ◽  
Philippe Gilotte ◽  
Yoann Eulalie ◽  
...  
Author(s):  
Edward A. Whalen ◽  
Doug S. Lacy ◽  
John C. Lin ◽  
Marlyn Y. Andino ◽  
Anthony E. Washburn ◽  
...  

2012 ◽  
Vol 134 (08) ◽  
pp. 55-55 ◽  
Author(s):  
G. Pechlivanoglou ◽  
C.N. Nayeri ◽  
C.O. Paschereit

This article discusses the performance optimization of wind turbine rotors with active flow control. An extensive multi-parameter investigation with a thorough matrix-grading system was performed to identify the most suitable solution for industrial quality, short/mid-term implementation on actual utility scale wind turbines. A very wide selection of aerodynamic flow control solutions was analyzed based on extensive multi-disciplinary literature review and through aerodynamic and aeroelastic simulations. It is suggested that the trailing edge devices have the most favorable performance in the field of system integration and mechanical design performance. Compliant structures like the flexible flap keep the number of moving parts to a minimum while maintaining high performance and manufacturing simplicity. The use of flexible and elastic materials based on polymers or rubber material improves the lightning strike resistance of these solutions and allows for low-cost large-scale production. The actuator principle, sensitivity, and reliability are decisive parameters, and pneumatic actuators seem to strike a good balance between performance, cost, and reliability.


2011 ◽  
Vol 48 (3) ◽  
pp. 786-796 ◽  
Author(s):  
Michael A. McVeigh ◽  
Hassan Nagib ◽  
Tom Wood ◽  
Israel Wygnanski

2019 ◽  
Vol 56 (4) ◽  
pp. 1376-1386 ◽  
Author(s):  
John C. Lin ◽  
Edward A. Whalen ◽  
Marlyn Y. Andino ◽  
Emilio C. Graff ◽  
Douglas S. Lacy ◽  
...  

Author(s):  
Ahmed Aly ◽  
Jonathan Colton

Active flow control devices have been proven to reduce drag and delay stall on commercial aircraft. This leads to lower fuel usage and thus reduced flight costs. However, there is a large uncertainty as to how to integrate active flow control devices into aircraft, specifically those with composite structures. In addition, the cost of manufacturing active flow control devices for large-scale production has not been previously studied. In this article, design concepts for the attachment of a fluidic oscillator to a composite aircraft structure are investigated. A systematic approach from the conceptual design to the final design is performed using different design tools. A cost analysis is performed to select the most cost-effective design configuration based on large volume fluidic oscillator production. Through design validation and cost estimation, the final design is shown to be feasible for large volume manufacturing.


Author(s):  
Edward A. Whalen ◽  
Marc Spoor ◽  
Paul M. Vijgen ◽  
John Tran ◽  
Arvin Shmilovich ◽  
...  

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