Active flow control and its applications in supersonic boundary layer Article Swipe
Boundary layer transition is a typical aerodynamic phenomenon in supersonic flow that refers to the transition of the boundary layer from laminar flow to turbulent flow. The instabilities and transition mechanisms are complicated. A turbulent boundary layer has an associated higher energy content more momentum and, therefore, is less prone to be separated. Furthermore, accurate and fast transition in the flow over the compressor blades in turbo machinery provides significant flow mixing, resulting in an increase in engine performance. In addition, the development of the scramjet made it possible to use plasma actuators as turbulator to increase the turbulence within an isolator and increase combustion efficiency. Thus, different methods of boundary layer transition have been proposed. The focus of this chapter is a low Reynolds number supersonic boundary layer and its interaction with an active flow control device. The Plasma-Based Actuator’s high repetition rate enables itself as an unsteady control mechanism to address the unsteady flow features. Moreover, its strong forcing makes it suitable for flow control applications in the high-speed flow regime, especially the supersonic boundary layer.
Related Topics
Concepts
Boundary layer
Mechanics
Flow separation
Supersonic speed
Boundary layer control
Plasma actuator
Turbulence
Choked flow
External flow
Boundary layer thickness
Flow control (data)
Aerospace engineering
Laminar flow
Materials science
Aerodynamics
Turbulator
Laminar-turbulent transition
Mach number
Reynolds number
Physics
Engineering
Dielectric barrier discharge
Optoelectronics
Dielectric
Telecommunications
Metadata
- Type
- book-chapter
- Language
- en
- Landing Page
- https://doi.org/10.5772/intechopen.1001967
- https://www.intechopen.com/citation-pdf-url/1146923
- OA Status
- hybrid
- References
- 22
- Related Works
- 10
- OpenAlex ID
- https://openalex.org/W4385341720
All OpenAlex metadata
Raw OpenAlex JSON
- OpenAlex ID
-
https://openalex.org/W4385341720Canonical identifier for this work in OpenAlex
- DOI
-
https://doi.org/10.5772/intechopen.1001967Digital Object Identifier
- Title
-
Active flow control and its applications in supersonic boundary layerWork title
- Type
-
book-chapterOpenAlex work type
- Language
-
enPrimary language
- Publication year
-
2023Year of publication
- Publication date
-
2023-07-24Full publication date if available
- Authors
-
Tian GanList of authors in order
- Landing page
-
https://doi.org/10.5772/intechopen.1001967Publisher landing page
- PDF URL
-
https://www.intechopen.com/citation-pdf-url/1146923Direct link to full text PDF
- Open access
-
YesWhether a free full text is available
- OA status
-
hybridOpen access status per OpenAlex
- OA URL
-
https://www.intechopen.com/citation-pdf-url/1146923Direct OA link when available
- Concepts
-
Boundary layer, Mechanics, Flow separation, Supersonic speed, Boundary layer control, Plasma actuator, Turbulence, Choked flow, External flow, Boundary layer thickness, Flow control (data), Aerospace engineering, Laminar flow, Materials science, Aerodynamics, Turbulator, Laminar-turbulent transition, Mach number, Reynolds number, Physics, Engineering, Dielectric barrier discharge, Optoelectronics, Dielectric, TelecommunicationsTop concepts (fields/topics) attached by OpenAlex
- Cited by
-
0Total citation count in OpenAlex
- References (count)
-
22Number of works referenced by this work
- Related works (count)
-
10Other works algorithmically related by OpenAlex
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| referenced_works | https://openalex.org/W2166911839, https://openalex.org/W2098482200, https://openalex.org/W2167404440, https://openalex.org/W3101956843, https://openalex.org/W2004840352, https://openalex.org/W2179070831, https://openalex.org/W2776016772, https://openalex.org/W2114473945, https://openalex.org/W2068921760, https://openalex.org/W2077244043, https://openalex.org/W2001148058, https://openalex.org/W2588244242, https://openalex.org/W2099683461, https://openalex.org/W1974179699, https://openalex.org/W2756453977, https://openalex.org/W2317043713, https://openalex.org/W2598579942, https://openalex.org/W2144603599, https://openalex.org/W2046936957, https://openalex.org/W2066620839, https://openalex.org/W2990949894, https://openalex.org/W2781592890 |
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