Improved Effectiveness of Vane-Type Vortex Generators for Incident Shock-Induced Separation

An experimental investigation is conducted to improve the control effectiveness of an array of vane-type vortex generators (VG) implemented 6 [Formula: see text] upstream of an incident shock-induced separation generated using a 14-deg wedge in a Mach 2.05 flow. Initially, the effect of an array of rectangular vanes (RRV) is studied by varying the vane 1) chord to height [Formula: see text], 4.2, 2) angle [Formula: see text], 20, 18, and 16 deg, 3) height to boundary-layer thickness [Formula: see text], 0.5, 0.3, and 0.2, and 4) interdevice spacing to height [Formula: see text], 9.5, 7.5, 6.5, 5.7, 5.5, and 5.0. Similar tests were also performed for ramp vanes (RV) with [Formula: see text]. Due to inherent design differences, an RRV device generates a larger region of vortex influence relative to an RV device. Therefore, reducing [Formula: see text] significantly reduces the extent of uncontrolled separation regions between neighboring VGs that improves their separation control capability. The best performing RRV devices with vane height [Formula: see text], [Formula: see text], and [Formula: see text] show maximum reduction in separation extent of nearly 80, 74, and 70%, respectively, relative to no control. The equivalent RV devices, however, show much reduced control effectiveness. All controls exhibit a shift in the dominant separation frequency to higher values, indicating a reduction in the overall extent of separation.

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Publication Details

Journal
AIAA Journal
Published
2024-09-02
DOI
https://doi.org/10.2514/1.j064000
Citations
2
Primary Topic
Combustion and Detonation Processes
Type
article
Field-Weighted Citation Impact
2.60
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article

Improved Effectiveness of Vane-Type Vortex Generators for Incident Shock-Induced Separation

Saurabh Verma, C. Manisankar
2 citations
AIAA Journal
Combustion and Detonation Processes
2.60
article

Improved Effectiveness of Vane-Type Vortex Generators for Incident Shock-Induced Separation

Saurabh Verma, C. Manisankar
article en
2 citations

Abstract

An experimental investigation is conducted to improve the control effectiveness of an array of vane-type vortex generators (VG) implemented 6 [Formula: see text] upstream of an incident shock-induced separation generated using a 14-deg wedge in a Mach 2.05 flow. Initially, the effect of an array of rectangular vanes (RRV) is studied by varying the vane 1) chord to height [Formula: see text], 4.2, 2) angle [Formula: see text], 20, 18, and 16 deg, 3) height to boundary-layer thickness [Formula: see text], 0.5, 0.3, and 0.2, and 4) interdevice spacing to height [Formula: see text], 9.5, 7.5, 6.5, 5.7, 5.5, and 5.0. Similar tests were also performed for ramp vanes (RV) with [Formula: see text]. Due to inherent design differences, an RRV device generates a larger region of vortex influence relative to an RV device. Therefore, reducing [Formula: see text] significantly reduces the extent of uncontrolled separation regions between neighboring VGs that improves their separation control capability. The best performing RRV devices with vane height [Formula: see text], [Formula: see text], and [Formula: see text] show maximum reduction in separation extent of nearly 80, 74, and 70%, respectively, relative to no control. The equivalent RV devices, however, show much reduced control effectiveness. All controls exhibit a shift in the dominant separation frequency to higher values, indicating a reduction in the overall extent of separation.

AIAA JournalVol. 62(11)
National Aerospace Laboratories (IN), Council of Scientific and Industrial Research (IN)
Openalex Percentile: Top 8%
Combustion and Detonation Processes
2.60
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