Interpretation of wake instability at slip line in rotating detonation. Issue 8 (21st October 2018)
- Record Type:
- Journal Article
- Title:
- Interpretation of wake instability at slip line in rotating detonation. Issue 8 (21st October 2018)
- Main Title:
- Interpretation of wake instability at slip line in rotating detonation
- Authors:
- Liu, Pengxin
Li, Qin
Huang, Zhangfeng
Zhang, Hanxin - Abstract:
- ABSTRACT: In studies on instabilities of flowfield in rotating detonation, one of the most common concerns is the instability at the slip line originating from the conjunction of the detonation wave and oblique shock. Using Euler equations associated with the 7-species-and-8-reaction finite-rate chemical reaction model of hydrogen/air mixtures, further studies are performed to simulate the 2-D rotating detonation, and the flow mechanism of instability at the slip line is investigated in depth. The results show that the distinct wake profile exists at the slip line, which is different from the typical mixing layer. Analysis indicates that the generation of wake is caused by the transition shock between the detonation wave and oblique shock. Because of the wake profile, the vorticity distribution therein appears in a double-layer layout, and different evolutions exist in different vorticity layers. Based on the velocity profile across the slip line, the analysis by the linear stability theory is made, and two main unstable modes which have different shape profiles and phase velocities are found. Discrete Fourier transformation is utilised to analyse the numerical results, and similar shape profiles are obtained. A general coincidence in velocity of vortex movement is also attained between the theoretical predictions and simulations. Investigations show that the wake instability is responsible for the unstable mechanism, and corresponding unstable structures differ from theABSTRACT: In studies on instabilities of flowfield in rotating detonation, one of the most common concerns is the instability at the slip line originating from the conjunction of the detonation wave and oblique shock. Using Euler equations associated with the 7-species-and-8-reaction finite-rate chemical reaction model of hydrogen/air mixtures, further studies are performed to simulate the 2-D rotating detonation, and the flow mechanism of instability at the slip line is investigated in depth. The results show that the distinct wake profile exists at the slip line, which is different from the typical mixing layer. Analysis indicates that the generation of wake is caused by the transition shock between the detonation wave and oblique shock. Because of the wake profile, the vorticity distribution therein appears in a double-layer layout, and different evolutions exist in different vorticity layers. Based on the velocity profile across the slip line, the analysis by the linear stability theory is made, and two main unstable modes which have different shape profiles and phase velocities are found. Discrete Fourier transformation is utilised to analyse the numerical results, and similar shape profiles are obtained. A general coincidence in velocity of vortex movement is also attained between the theoretical predictions and simulations. Investigations show that the wake instability is responsible for the unstable mechanism, and corresponding unstable structures differ from the canonical ones in typical mixing layers. … (more)
- Is Part Of:
- International journal of computational fluid dynamics. Volume 32:Issue 8/9(2018)
- Journal:
- International journal of computational fluid dynamics
- Issue:
- Volume 32:Issue 8/9(2018)
- Issue Display:
- Volume 32, Issue 8/9 (2018)
- Year:
- 2018
- Volume:
- 32
- Issue:
- 8/9
- Issue Sort Value:
- 2018-0032-NaN-0000
- Page Start:
- 379
- Page End:
- 394
- Publication Date:
- 2018-10-21
- Subjects:
- Rotating detonation -- slip line -- Kelvin–Helmholtz instability -- wake instability
Fluid dynamics -- Data processing -- Periodicals
532.05 - Journal URLs:
- http://www.tandfonline.com/toc/gcfd20/current ↗
http://www.tandfonline.com/ ↗ - DOI:
- 10.1080/10618562.2018.1533634 ↗
- Languages:
- English
- ISSNs:
- 1061-8562
- Deposit Type:
- Legaldeposit
- View Content:
- Available online (eLD content is only available in our Reading Rooms) ↗
- Physical Locations:
- British Library DSC - 4542.173705
British Library DSC - BLDSS-3PM
British Library STI - ELD Digital store - Ingest File:
- 9604.xml