Mechanika
86 (1/14), DOI: 10.7862/rm.2014.16
Transonic axial compressor active boundary layer control concept and its evaluation
Bartosz Ziegler
DOI: 10.7862/rm.2014.16
Abstract
The article presents a concept of boundary layer control in transonic axial compressors. Two methods for obtaining boundary layer control are presented. It is proposed that by combining those two methods, an efficient way of preventing turbulent boundary layer separation in transonic compressor passages can be obtained without the loss of the compressor flux. The concept, is based on the idea of removing boundary layer flows at one stage, and using this removed flux as a blowing type boundary layer control, at previous stage where lower pressures occur. This creates a loop of secondary flow between those stages preventing the boundary layer separation (especially the shock induced separation) on both stages. Two dimensional numerical analyses are performed to assess the possible passage performance (especially the diffusion factor). On the basis of two dimensional analyses, the possible performance of such compressor stage is estimated. The aerodynamic possibility of greatly increasing the axial compressing stage loadings and pressure ratios without increasing blade velocities and passage flow Mach numbers is shown. This possibility has a growing importance as the overall pressure ratio of turbojet engines and tends to rise with every next engine generation. Main conclusions are drawn, showing the possibilities for further research in the scope of this concept.
References
- Kerrebrock J. : Final Technical Report on AFOSR Grant F49620-98-1-0493 entitled RESEARCH AND DEVELOPMENT ON ASPIRATED COMPRESSORS, Gas Turbine Laboratory Department of Aeronautics and Astronautics MIT, Cambridge 2003.
- Epstein A. et al. : Final Technical Report on AFOSR Grant F49620-03-1-0309 entitled ASPIRATED HIGH PRESSURE COMPRESSOR, Gas Turbine Laboratory Department of Aeronautics and Astronautics MIT, Cambridge 2006.
- Knapke R.D., Turner M.G.: Detailed Unsteady Simulation of a Counterrotating Aspirated Compressor with a Focus on the Aspiration Slot and Plenum, Int. J. Rotating Machinery, 2013, Article ID 857617.
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About this Article
TITLE:
Transonic axial compressor active boundary layer control concept and its evaluation
AUTHORS:
Bartosz Ziegler
AUTHORS AFFILIATIONS:
Poznań University of Technology, ul. Piotrowo 3, 60-695 Poznań
JOURNAL:
Mechanika
86 (1/14)
KEY WORDS AND PHRASES:
flow separation, transonic diffusers, turbojet engines
FULL TEXT:
http://doi.prz.edu.pl/pl/pdf/mechanika/77
DOI:
10.7862/rm.2014.16
URL:
http://dx.doi.org/10.7862/rm.2014.16
RECEIVED:
2014-05-15
COPYRIGHT:
Publishing House of Rzeszow University of Technology Powstańców Warszawy 12, 35-959 Rzeszow