Transmission and reflection of sound by a blade row-Reference-Cited by-同舟云学术

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Transmission and reflection of sound by a blade row

Published:1971-01-25 Issue: Volume: Page:
ISSN:
Container-title:9th Aerospace Sciences Meeting
language:
Short-container-title:

Author:

AMIET R.¹

Affiliation:

1. UNITED AIRCRAFT RESEARCH LABS., EAST HARTFORD, CONN.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1971-181

Reference10 articles.

1. Amiet, R, Blld Sears, w.R. '"Re.rlectioo. and TrMmissioo of Oblique $01.md Wa-veby a Bl.ad• Ra.i," Basic AerOO}"lllimic Raise Research, Ir& Schwart,•d., NASASP-207, 1%9, PP- 223-230.

2. Durand, w. F., ed., Aer.od:nc Theo.ry, Vol.II, Dov!i!'.r' f'ublicat.ians, fnc., 196-3:pp.91-96.

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1. Comprehensive experimental investigation of mode transmission through stator vane rows: Results and calibration of an analytical prediction model;23rd AIAA/CEAS Aeroacoustics Conference;2017-06-02

2. Comparative study of different analytical approaches for modelling the transmission of sound waves through turbomachinery stators;22nd AIAA/CEAS Aeroacoustics Conference;2016-05-27

3. Numerical simulation of multistage turbine sound generation and propagation;Aerospace Science and Technology;2005-03

4. Simulation of noise generation due to blade row interaction in a high speed compressor;Aerospace Science and Technology;2004-06

5. The role of rotor blade blockage in the propagation of fan noise interaction tones;2nd Aeroacoustics Conference;1975-03-24

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