Experimental research on the shock wave control based on one power supply driven plasma synthetic jet actuator array. (June 2020)
- Record Type:
- Journal Article
- Title:
- Experimental research on the shock wave control based on one power supply driven plasma synthetic jet actuator array. (June 2020)
- Main Title:
- Experimental research on the shock wave control based on one power supply driven plasma synthetic jet actuator array
- Authors:
- Zhang, Zhibo
Zhang, Xiaoning
Wu, Yun
Jia, Min
Jin, Di
Sun, Zhengzhong
Li, Yinghong - Abstract:
- Abstract: The interaction between a ramp induced shock wave and a plasma synthetic jet actuator (PSJA) array was experimentally investigated using high-speed schlieren imaging technique. The PSJA array consisting of 10 actuators was driven by only one power supply. To enhance the actuation intensity, the actuators were located along the streamwise direction to form an accumulation effect. Experimental results showed that the plasma synthetic jet can penetrate into the supersonic flow field with a depth of more than 10 mm. Both the induced shock and the controlling gas bulbs generated by PSJA array can affect the shock wave. The separation shock wave bifurcates when interacting with the shock induced by the actuator. The foot portion of the separation shock wave disappeared when the controlling gas bulbs passed through the interaction region. What's more, as the actuators were located in streamwise direction, the controlling gas bulbs were completely emerged as a much larger gas bulb. As a result, the effective control time was longer than the single actuator and the control effect is also much better. Highlights: A novel method using streamwise plasma synthetic jet actuator array was proposed to control the ramp induced shock wave. The plasma synthetic jet actuator array consisted of 10 actuators was driven by only one power supply. The accumulation and convection of controlling gas bulbs and interaction with shockwave is the main control mechanism.
- Is Part Of:
- Acta astronautica. Volume 171(2020)
- Journal:
- Acta astronautica
- Issue:
- Volume 171(2020)
- Issue Display:
- Volume 171, Issue 2020 (2020)
- Year:
- 2020
- Volume:
- 171
- Issue:
- 2020
- Issue Sort Value:
- 2020-0171-2020-0000
- Page Start:
- 359
- Page End:
- 368
- Publication Date:
- 2020-06
- Subjects:
- Plasma synthetic jet -- Active flow control -- Shock wave -- Shock wave/boundary layer interaction -- Actuator array
Astronautics -- Periodicals
Outer space -- Exploration -- Periodicals
Astronautics
Periodicals
629.405 - Journal URLs:
- http://www.sciencedirect.com/science/journal/00945765 ↗
http://www.elsevier.com/journals ↗ - DOI:
- 10.1016/j.actaastro.2020.03.035 ↗
- Languages:
- English
- ISSNs:
- 0094-5765
- Deposit Type:
- Legaldeposit
- View Content:
- Available online (eLD content is only available in our Reading Rooms) ↗
- Physical Locations:
- British Library DSC - 0596.750000
British Library DSC - BLDSS-3PM
British Library HMNTS - ELD Digital store - Ingest File:
- 13396.xml