Study of the Effect of a Blade Tip Notch Damage on the Aerodynamic Performance of Transonic Compressor Rotors

Author:

Tang J.,Zhong Z. H.,Lu X.,Wang L. W.

Publisher

Pleiades Publishing Ltd

Reference34 articles.

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2. Chang, S., et al., Study on the external object damage law of aero-engine compressor blade, J. Mech. Eng., 2019, vol. 13, pp. 87–94.

3. Civil Aviation Administration of China. Chinese civil aviation regulations[S], Beijing: Civil Aviation Administration of China, 2021, pp. 42–52.

4. Bo, L., et al., Optimal design of non-axisymmetric end wall shape for transonic axial flow compressors, Propul. Technol., 2012, vol. 5, pp. 689–694.

5. Du, W.H., Analysis of flow losses in transonic axial flow compressors, Propul. Technol., 2008, vol. 3, pp. 339–343.

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