References
- Walter S. Cunnan, Wiliam Stevans, and Donald C. Urasek, 'Design and Perforrnance of a 427 Meter Per Second Tip Speed Two-Stage Fan Having a 2.40 Pressure Ratio,' NASA TP 1314, 1978
- Royce D. Moore, Lonnie Reid, 'Perfonnance of Single Stage Axial-F1ow Transonic Compressor and Stator Aspect Ratios of 1.63 and 1.78, Respectively, and With Design Pressure of 1.82,' NASA TP 1974, 1982
- Ronald J. Steinke， 'Design of 9.271 Pressure Ratio Five Stage Core Compressor and Overall Perfonnance for First Three Stages,' NASA TP 2597, 1986
- 'Designing Compressors with Concepts NREC', Concepts ETI, 2007
- Shuo Li, 'Design Turbomachine Using AxCent,' Concepts ETI, 2009
Cited by
- vol.13, pp.1, 2010, https://doi.org/10.5293/KFMA.2010.13.1.059
- Experimental Research on Multi Stage Transonic Axial Compressor Performance Evaluation vol.14, pp.6, 2011, https://doi.org/10.5293/kfma..2011.14.6.096
- Transient performance prediction of an axial compressor considering VIGV operation speeds vol.28, pp.10, 2014, https://doi.org/10.1007/s12206-014-0923-7