Author:
Yang Yong,Xiang Honghui,Gao Jie,Xu Kaijun,Yang Rongfei,Ge Ning
Publisher
Springer Science and Business Media LLC
Reference20 articles.
1. Pratt T.K., Seitelman L.H., Zampano R.R., et al., Optimization applications for aircraft engine design and manufacture. Advances in Engineering Software, 1993, 16(2): 111–117.
2. Broichhausen K.D., Ziegler K.U., Supersonic and transonic compressors: past, status and technology trends. ASME Turbo Expo, Nevada, USA, 2005, 6: 63–74. DOI: https://doi.org/10.1115/GT2005-69067.
3. Miller R.J., Moss R.W., Ainsworth R.W., et al., Time resolved vane rotor interaction in a high pressure turbine stage. Journal of Turbomachinery, 2003, 125(1): 1–13.
4. Wang Y.F., Hu J., Li C.P., et al., Effects of up-stream rotor on the aerodynamic force on down-stream stator blades. Acta Aeronauticaet Astronautica Sinica, 2006, 27(4): 545–550. (in Chinese)
5. Dudzinski T.J., Krause L.N., Effect of inlet geometry on flow-angle characteristics of miniature total pressure tubes. Technical Report, Report No.NASA-TN-D-6406, 1971.
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