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Transition control of the Blasius boundary layer using passivity
- Source :
- Aerospace Systems. 2:21-31
- Publication Year :
- 2018
- Publisher :
- Springer Science and Business Media LLC, 2018.
-
Abstract
- The control problem for linearised three-dimensional perturbations about a nominal laminar boundary layer over a flat plate (the Blasius profile) is considered. With a view to preventing the laminar to turbulent transition, appropriate inputs, outputs, and feedback controllers are synthesised that can be used to stabilise the system. The linearised Navier–Stokes equations are reduced to the Orr–Sommerfeld and Squire equations with wall-normal velocity actuation entering through the boundary conditions on the wall. An analysis of the work-energy balance is used to identify an appropriate sensor output that leads to a passive system for certain values of the streamwise and spanwise wavenumbers. Even when the system is unstable, it is demonstrated that strictly positive real feedback can stabilise this system using the special output.
- Subjects :
- 0209 industrial biotechnology
Turbulence
Mechanical Engineering
Passivity
Control (management)
Aerospace Engineering
Laminar flow
02 engineering and technology
Mechanics
01 natural sciences
010305 fluids & plasmas
Physics::Fluid Dynamics
Boundary layer
020901 industrial engineering & automation
Space and Planetary Science
Control and Systems Engineering
0103 physical sciences
Blasius boundary layer
Wavenumber
Boundary value problem
Computers in Earth Sciences
Social Sciences (miscellaneous)
Mathematics
Subjects
Details
- ISSN :
- 25233955 and 25233947
- Volume :
- 2
- Database :
- OpenAIRE
- Journal :
- Aerospace Systems
- Accession number :
- edsair.doi...........a92fa737057e1623659ff84dc9cbb360
- Full Text :
- https://doi.org/10.1007/s42401-018-0021-0