Using a shock control bump to improve the performance of an axial compressor blade section
Author:
Publisher
Springer Science and Business Media LLC
Subject
General Physics and Astronomy,Mechanical Engineering
Link
http://link.springer.com/content/pdf/10.1007/s00193-016-0672-x.pdf
Reference28 articles.
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3. Biollo, R., Benini, E.: Recent advances in transonic axial compressor aerodynamics. Prog. Aerosp. Sci. 56, 1–18 (2013)
4. Wang, D.X., He, L., Li, Y.S., Wells, R.G.: Adjoint aerodynamic design optimization for blades in multistage turbomachines—Part II: Validation and application. J. Turbomach. 132(2), 021012 (11 pp) (2010)
5. Lian, Y., Liou, M.S.: Multi-objective optimization of transonic compressor blade using evolutionary algorithm. J. Propuls. Power 21(6), 979–987 (2005)
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