Pulsed jet actuators for suppressing flow separation

Author(s):  
K. McManus ◽  
A. Ducharme ◽  
C. Goldey ◽  
J. Magill
Fluids ◽  
2021 ◽  
Vol 6 (4) ◽  
pp. 166
Author(s):  
Stephan Löffler ◽  
Carola Ebert ◽  
Julien Weiss

The control of flow separation on aerodynamic surfaces remains a fundamental goal for future air transportation. On airplane wings and control surfaces, the effects of flow separation include decreased lift, increased drag, and enhanced flow unsteadiness and noise, all of which are detrimental to flight performance, fuel consumption, and environmental emissions. Many types of actuators have been designed in the past to counter the negative effects of flow separation, from passive vortex generators to active methods like synthetic jets, plasma actuators, or sweeping jets. At the Chair of Aerodynamics at TU Berlin, significant success has been achieved through the use of pulsed jet actuators (PJA) which operate by ejecting a given amount of fluid at a specified frequency through a slit-shape slot on the test surface, thereby increasing entrainment and momentum in a separating boundary layer and thus delaying flow separation. Earlier PJAs were implemented using fast-switching solenoid valves to regulate the jet amplitude and frequency. In recent years, the mechanical valves have been replaced by fluidic oscillators (FO) in an attempt to generate the desired control authority without any moving parts, thus paving the way for future industrial applications. In the present article, we present in-depth flow and design analysis which affect the operation of such FO-based PJAs. We start by reviewing current knowledge on the mechanism of flow separation control with PJAs before embarking on a detailed analysis of single-stage FO-based PJAs. In particular, we show that there is a fundamental regime where the oscillation frequency is mainly driven by the feedback loop length. Additionally, there are higher-order regimes where the oscillation frequency is significantly increased. The parameters that influence the oscillation in the different regimes are discussed and a strategy to incorporate this new knowledge into the design of future actuators is proposed.


1995 ◽  
Author(s):  
K McManus ◽  
P Joshi ◽  
H Legner ◽  
S Davis

Energies ◽  
2019 ◽  
Vol 12 (4) ◽  
pp. 587 ◽  
Author(s):  
Weiyu Lu ◽  
Guoping Huang ◽  
Jinchun Wang ◽  
Yuxuan Yang

Unsteady flow separation controls are effective in suppressing flow separations. However, the unique phenomena in unsteady separation control, including frequency-dependent, threshold, location-dependent, and lock-on effects, are not fully understood. Furthermore, the mechanism of the effectiveness that lies in unsteady flow controls remains unclear. Thus, this study aims to interpret further the unique phenomena and mechanism in unsteady flow separation controls. First, numerical simulation and some experimental results of a separated curved diffuser using pulsed jet flow control are discussed to show the four unique phenomena. Second, the bases of unsteady flow control, flow instability, and free shear flow theories are introduced to elucidate the unique phenomena and mechanism in unsteady flow separation controls. Subsequently, with the support of these theories, the unique phenomena of unsteady flow control are interpreted, and the mechanisms hidden in the phenomena are revealed.


Author(s):  
Marlyn Y. Andino ◽  
John C. Lin ◽  
Anthony E. Washburn ◽  
Edward A. Whalen ◽  
Emilio C. Graff ◽  
...  

Author(s):  
Jianfeng Zhu ◽  
Guoping Huang ◽  
Xin Fu ◽  
Yong Fu ◽  
Haibin Yu

This paper presents a micro pulsed aspirated jet concept to suppress the flow separation in compressors. According to this concept, a kind of pulsed jet and an imitating cascade channel has been established; the characteristic frequency of separation vortex is about 266Hz. The experimental and numerical investigation about the unsteady frequency has been finished, and when the frequency of pulsed jet is close to the characteristic frequency of separation vortex, the control effects are more obvious. Based on the numerical results, the proper orthogonal decomposition (POD) method is introduced to analyze the unsteady control mechanism, and the spatial and temporal structure of unsteady flow field can be decoupled by POD method. The POD analysis results show that the main effect of unsteady pulsed jet is reallocating the energy of each mode, and selectively strengthening or weakening certain modes; the effect of steady jet is overall reducing the energy of high order modes. Based on the reasonable control parameters of pulsed jet, the energy in higher modes will be transferred to the average flow mode, and the translation of modal energy is coming from the reconstructing of spatial flow structures and the ordering of modal evolution characteristic. Finally, the validation of experimental investigation has been finished; and the credibility of the analysis is also enhanced.


2007 ◽  
Vol 78 (3-4) ◽  
pp. 255-281 ◽  
Author(s):  
Clyde Warsop ◽  
Martyn Hucker ◽  
Andrew J. Press ◽  
Paul Dawson

Author(s):  
Peter Scholz ◽  
Jens Ortmanns ◽  
Christian Kahler ◽  
Rolf Radespiel

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