Open Access
Issue
MATEC Web Conf.
Volume 108, 2017
2017 International Conference on Mechanical, Aeronautical and Automotive Engineering (ICMAA 2017)
Article Number 08008
Number of page(s) 5
Section Power System and Mechatronics
DOI https://doi.org/10.1051/matecconf/201710808008
Published online 31 May 2017
  1. Nikuradse J. Laws of flow in rough pipes[C]//VDI Forschungsheft. (1933) [Google Scholar]
  2. Schlichting H. Experimentelle untersuchungen zum rauhigkeitsproblem [J].Archive of Applied Mechanics, 7(1): 1–34 (1936) [Google Scholar]
  3. Bammert K, Milsch R. Boundary layers on rough compressor blades[C]//ASME 1972 International Gas Turbine and Fluids Engineering Conference and Products Show. American Society of Mechanical Engineers, (1972), V001T01A047-V001T01A047 [Google Scholar]
  4. Syverud E, Brekke O, Bakken L E. Axial compressor deterioration caused bysaltwater ingestion[C]//ASME Turbo Expo 2005: Power for Land, Sea, and Air. American Society of Mechanical Engineers, 327–337 (2005) [CrossRef] [Google Scholar]
  5. Syverud E, Bakken L E. The impact of surface roughness on axial compressor performance deterioration[C]//ASME Turbo Expo 2006: Power for Land, Sea, and Air. American Society of Mechanical Engineers, 491–501 (2006) [Google Scholar]
  6. Suder K L, Chima R V, Strazisar A J, et al. The effect of adding roughness and thickness to a transonic axial compressor rotor[C]//ASME 1994 International Gas Turbine and Aeroengine Congress and Exposition. American Society of Mechanical Engineers, (1994), V001T01A113-V001T01A113 [Google Scholar]
  7. MoriniM, Pinelli M, Spina P R, et al. Computational fluid dynamics simulation of fouling on axial compressor stages[J]. Journal of Engineering for Gas Turbines and Power, 132(7): 072401 (2010) [CrossRef] [Google Scholar]
  8. Chen S, Zhang C, Shi H, et al. Numerical Study on the Impact of Fouling on Axial Compressor Stages [J]. Journal of Propulsion Technology, 3: 006 (2012) [Google Scholar]
  9. Shi H, Chen SW, Zhang C, et al. Numerical simulation of fouling deposition in compressor rotor[J]. Journal of Aerospace Power, 27(5): 1061–1067 (2012) [Google Scholar]
  10. Reid L, Moore R D. Design and overall performance of four highly loaded, high speed inlet stages for an advanced high-pressure-ratio core compressor[J]. (1978) [Google Scholar]
  11. ANSYS CFX. Version 14.0[J]. Ansys Inc, (2011) [Google Scholar]

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