Abstract

The low-frequency pressure pulsations in a large low-speed open jet wind tunnel were studied using a 1:20 scaled model wind tunnel. It was found that plane pressure standing waves existed in all three directions of the wind tunnel’s plenum. It was confirmed that the large pressure pulsations in the transverse direction of the plenum were caused by the resonance of the plane pressure standing waves in that direction with the edgetone feedback (vortex-sound feedback between the nozzle and the collector). The analysis of the standing waves in the vertical direction of the plenum suggested that they might come from self-excited oscillations. For the model wind tunnel with a 1:20 strictly scaled collector, the standing waves in the transverse direction of the plenum were much stronger than those in the other two directions. By increasing the width of the collector, the intensity of the standing waves in the transverse direction was significantly reduced to a level similar to that of the standing waves in the vertical direction. It was also found that the standing waves in the transverse direction were significantly enhanced after a floor was added to the test section.

Highlights

  • Low-frequency pressure pulsation1 is a common phenomenon in open jet wind tunnels

  • It is believed that the low frequency pressure pulsations in open jet wind tunnels are attributed to the feedback oscillations generated by the interaction of the coherent vortices in the jet’s shear layer with the collector

  • The aim of this paper is to further investigate the standing wave and its impact on the pressure pulsations in the plenum of FL-17, based on a 1:20 scaled wind tunnel model (SKLA-01)

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Summary

INTRODUCTION

Low-frequency pressure pulsation is a common phenomenon in open jet wind tunnels. It is characterized by periodic lowfrequency pressure pulsations in the plenum of the wind tunnel over a specific range of test wind speeds.. It is believed that the low frequency pressure pulsations in open jet wind tunnels are attributed to the feedback oscillations generated by the interaction of the coherent vortices in the jet’s shear layer with the collector (referred to as the edgetone feedback or jet-collector feedback).. The feedback loop closes when the disturbance reaches the nozzle, modulating and influencing the shear layer destabilization process and causing a new vortex to be shed.2,5,8,12,17,21–25 This leads to low frequency pressure feedback pulsations in the jet and the plenum of the wind tunnel.

WIND TUNNEL TEST SETUP
DOMINANT FREQUENCIES IN THE PLENUM
STANDING WAVE CHARACTERISTICS OF DOMINANT PULSATIONS
The standing wave in transverse direction
The standing wave in vertical direction
Findings
CONCLUSIONS
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