Investigations on the Acoustic Resonance in Aeroengine Multi-Stage Compressor
Author:
Publisher
Springer Singapore
Link
https://link.springer.com/content/pdf/10.1007/978-981-33-6060-0_23
Reference21 articles.
1. Greitzer EM (1976) Surge and rotating stall in axial flow compressors—part II: experimental results and comparison with theory. J Eng Gas Turbines Power 98(2): 199
2. Beselt C et al (2012) Experimental and numerical investigations of rotating instability phenomenon in an axial compressor stator. In: Proceedings of 42nd AIAA fluid dynamics conference and exhibit
3. Lin Z, Li K, Yang S (2010) Experimental research on sound waves excitation to aero-engine compressor rotor blade. J Dyn Control 008(1):12–18
4. Parker R (1968) An investigation of acoustic resonance effects in an axial flow compressor stage. J Sound Vib 8(2):281–297
5. Kameier F, Nawrot T, Neise W (1992) Experimental investigation of tip clearance noise in axial flow machines. in DGLR—AIAA 14th Aeroacoustics Conference
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