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Open Access

Investigation of pressure wave behaviors in the rotational speed effects on a pressure-exchange wave rotor

Shining CHANa,bHuoxing LIUc( )Hang SONGdFengchao LIeChongwen JIANGa,bZhenxun GAOa,b
Aircraft & Propulsion Laboratory, Ningbo Institute of Technology, Beihang University, Ningbo 315800, China
National Laboratory for Computational Fluid Dynamics, School of Aeronautic Science and Engineering, Beihang University, Beijing 100083, China
Research Institute of Aero-Engine, Beihang University, Beijing 100083, China
AVIC CAPDI Integration Equipment Co., Ltd., Beijing 102206, China
Aero Engine Academy of China, Beijing 101300, China

Peer review under responsibility of Editorial Committee of CJA.

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Abstract

A wave rotor is suitable for compact and efficient pressure-exchange between gas flows. This work measured the circumferential pressure distribution of the rotor/stator interfaces and utilized a CFD method to simulate the unsteady pressure waves. The experimental and CFD results showed some slopes in the circumferential pressure distributions, and the slopes indicated the traces of specific unsteady pressure waves. Such traces varied regularly if the rotational speed varied within a range from −11% to +11% off the baseline value, but they were seriously disturbed if the rotational speed varied by −45% from the baseline value. It verified that a pressure wave in a wave rotor tended to keep its pressure ratio and propagation velocity unchanged if the rotational speed varied by a small extent, and that the pressure wave could not keep its propagation patterns if the rotational speed varied by a large extent. Because of the pressure wave behaviors, the wave rotor demonstrated specific regulations of the rotational speed effects on its operational states.

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Chinese Journal of Aeronautics
Pages 247-259

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Cite this article:
CHAN S, LIU H, SONG H, et al. Investigation of pressure wave behaviors in the rotational speed effects on a pressure-exchange wave rotor. Chinese Journal of Aeronautics, 2022, 35(5): 247-259. https://doi.org/10.1016/j.cja.2021.05.015

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Received: 12 September 2020
Revised: 09 October 2020
Accepted: 30 November 2020
Published: 04 July 2021
© 2022 Chinese Society of Aeronautics and Astronautics.

This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).