Evaluation Of The Vortex Generator Flow Control In The FOI-EIC-01 Inlet At Different Flight Conditions

2007 ◽  
Author(s):  
Adam Jirasek
Keyword(s):  
Flow Control ◽  
Vortex Generator

Steady Vortex-Generator Jet Flow Control on a Highly Loaded Transonic Low-Pressure Turbine Cascade: Effects of Compressibility and Roughness

2014 ◽  
Vol 136 (11) ◽  
Author(s):  
Chiara Bernardini ◽  
Stuart I. Benton ◽  
John D. Lee ◽  
Jeffrey P. Bons ◽  
Jen-Ping Chen ◽  
...  
Keyword(s):  
Surface Roughness ◽  
Mach Number ◽  
Flow Control ◽  
High Speed ◽  
Vortex Generator ◽  
Control Performance ◽  
Low Pressure Turbine ◽  
Blowing Ratio ◽  
Turbulent Separation ◽  
Mach Number Distribution

A new high-speed linear cascade has been developed for low-pressure turbine (LPT) studies at The Ohio State University. A compressible LPT profile is tested in the facility and its baseline performance at different operating conditions is assessed by means of isentropic Mach number distribution and wake total pressure losses. Active flow control is implemented through a spanwise row of vortex-generator jets (VGJs) located at 60% chord on the suction surface. The purpose of the study is to document the effectiveness of VGJ flow control in high-speed compressible flow. The effect on shock-induced separation is assessed by Mach number distribution, wake loss surveys and shadowgraph. Pressure sensitive paint (PSP) is applied to understand the three dimensional flow and shock pattern developing from the interaction of the skewed jets and the main flow. Data show that with increasing blowing ratio, the losses are first decreased due to separation reduction, but losses connected to compressibility effects become stronger due to increased passage shock strength and jet orifice choking; therefore, the optimum blowing ratio is a tradeoff between these counteracting effects. The effect of added surface roughness on the uncontrolled flow and on flow control behavior is also investigated. At lower Mach number, turbulent separation develops on the rough surface and a different flow control performance is observed. Steady VGJs appear to have control authority even on a turbulent separation but higher blowing ratios are required compared to incompressible flow experiments reported elsewhere. Overall, the results show a high sensitivity of steady VGJs control performance and optimum blowing ratio to compressibility and surface roughness.

Study on Flow Separation Control by Vortex Generator Jets with Different Parameters

2012 ◽  
Vol 588-589 ◽  
pp. 1786-1789
Author(s):  
Yong Hui Xie ◽  
Zhong Yang Shen ◽  
Tao Fan
Keyword(s):  
Flow Control ◽  
Flow Separation ◽  
Vortex Generator ◽  
Separation Control ◽  
Flow Separation Control ◽  
Profound Influence ◽  
Orthogonal Analysis ◽  
Conical Diffuser ◽  
Flow Charts ◽  
Vortex Generator Jets

In order to investigate the mechanism of flow separation control in conical diffuser by vortex generator jets (VGJs) method, numerical simulations were conducted to discuss the effect of VGJs with different parameters on flow control. The aerodynamic performance in conical diffuser with angle of 14° was tested and analyzed based on Shear-Stress-Transport (SST) simulation. The flow charts at several sections were analyzed, illuminating the formation of complex vortices. Moreover, the effects of 5 VGJs parameters on the diffuser were analyzed by orthogonal analysis. It was shown that the number of jets and the pitch angle of jet showed more profound influence on the flow control by VGJs.

Numerical study of micro-ramp vortex generator for supersonic ramp flow control at Mach 2.5

Shock Waves ◽  
2016 ◽  
Vol 27 (1) ◽  
pp. 79-96 ◽  
Author(s):  
Y. Yan ◽  
L. Chen ◽  
Q. Li ◽  
C. Liu
Keyword(s):  
Flow Control ◽  
Numerical Study ◽  
Vortex Generator

Evaluation and Parameterization of Round Vortex Generator Jet Experiments for Flow Control

AIAA Journal ◽  
2012 ◽  
Vol 50 (11) ◽  
pp. 2508-2524 ◽  
Author(s):  
Florian von Stillfried ◽  
Stefan Wallin ◽  
Arne V. Johansson ◽  
Marcus Casper ◽  
Jens Ortmanns
Keyword(s):  
Flow Control ◽  
Vortex Generator ◽  
Vortex Generator Jet

Design of Vortex Generator Flow Control in Inlets

2006 ◽  
Vol 43 (6) ◽  
pp. 1886-1892 ◽  
Author(s):  
Adam Jirásek
Keyword(s):  
Flow Control ◽  
Vortex Generator

scholarly journals Experimental Studies of Active and Passive Flow Control Techniques Applied in a Twin Air-Intake

2013 ◽  
Vol 2013 ◽  
pp. 1-8 ◽  
Author(s):  
Akshoy Ranjan Paul ◽  
Shrey Joshi ◽  
Aman Jindal ◽  
Shivam P. Maurya ◽  
Anuj Jain
Keyword(s):  
Flow Control ◽  
Pitch Angle ◽  
Pressure Loss ◽  
Total Pressure ◽  
Static Pressure ◽  
Vortex Generator ◽  
Performance Characteristics ◽  
Total Pressure Loss ◽  
Air Intake ◽  
Side Walls

The flow control in twin air-intakes is necessary to improve the performance characteristics, since the flow traveling through curved and diffused paths becomes complex, especially after merging. The paper presents a comparison between two well-known techniques of flow control: active and passive. It presents an effective design of a vortex generator jet (VGJ) and a vane-type passive vortex generator (VG) and uses them in twin air-intake duct in different combinations to establish their effectiveness in improving the performance characteristics. The VGJ is designed to insert flow from side wall at pitch angle of 90 degrees and 45 degrees. Corotating (parallel) and counterrotating (V-shape) are the configuration of vane type VG. It is observed that VGJ has the potential to change the flow pattern drastically as compared to vane-type VG. While the VGJ is directed perpendicular to the side walls of the air-intake at a pitch angle of 90 degree, static pressure recovery is increased by 7.8% and total pressure loss is reduced by 40.7%, which is the best among all other cases tested for VGJ. For bigger-sized VG attached to the side walls of the air-intake, static pressure recovery is increased by 5.3%, but total pressure loss is reduced by only 4.5% as compared to all other cases of VG.

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