Numerical evaluation of heat exchange mechanism by slit resonators

Youhi Morii; Kazuto Kuzuu; Taro Shimizu

Numerical evaluation of heat exchange mechanism by slit resonators

Youhi Morii, Kazuto Kuzuu, Taro Shimizu

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

Abstract

The characteristic of the heat exchange mechanism by slit resonators is numerically investigated. In general, a rocket engine chamber is filled with hot gas, and slit resonators, which are equipped outside of the chamber wall near faceplate, are filled with cold gas. Therefore, when the resonators work well, the cold gas in the resonator might be exchanged for the hot gas in the rocket engine because of acoustic oscillations or vortex generations and motions. In this paper, the heat exchange mechanism by the slit resonators is numerically evaluated on the effect of intensity of incident wave, slit resonator shapes, and kinematic viscosity. In addition, the new idea of a slit resonator shape for the suppression of the heat exchange and its damping performance are mentioned.

Original language	English
Title of host publication	49th AIAA/ASME/SAE/ASEE Joint PropulsionConference
Publication status	Published - 2013 Sep 16
Externally published	Yes
Event	49th AIAA/ASME/SAE/ASEE Joint PropulsionConference - San Jose, CA, United States Duration: 2013 Jul 14 → 2013 Jul 17

Publication series

Name	49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference

Other

Other	49th AIAA/ASME/SAE/ASEE Joint PropulsionConference
Country/Territory	United States
City	San Jose, CA
Period	13/7/14 → 13/7/17

ASJC Scopus subject areas

Aerospace Engineering
Control and Systems Engineering
Electrical and Electronic Engineering

Cite this

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title = "Numerical evaluation of heat exchange mechanism by slit resonators",

abstract = "The characteristic of the heat exchange mechanism by slit resonators is numerically investigated. In general, a rocket engine chamber is filled with hot gas, and slit resonators, which are equipped outside of the chamber wall near faceplate, are filled with cold gas. Therefore, when the resonators work well, the cold gas in the resonator might be exchanged for the hot gas in the rocket engine because of acoustic oscillations or vortex generations and motions. In this paper, the heat exchange mechanism by the slit resonators is numerically evaluated on the effect of intensity of incident wave, slit resonator shapes, and kinematic viscosity. In addition, the new idea of a slit resonator shape for the suppression of the heat exchange and its damping performance are mentioned.",

author = "Youhi Morii and Kazuto Kuzuu and Taro Shimizu",

year = "2013",

month = sep,

day = "16",

language = "English",

isbn = "9781624102226",

series = "49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference",

booktitle = "49th AIAA/ASME/SAE/ASEE Joint PropulsionConference",

note = "49th AIAA/ASME/SAE/ASEE Joint PropulsionConference ; Conference date: 14-07-2013 Through 17-07-2013",

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TY - GEN

T1 - Numerical evaluation of heat exchange mechanism by slit resonators

AU - Morii, Youhi

AU - Kuzuu, Kazuto

AU - Shimizu, Taro

PY - 2013/9/16

Y1 - 2013/9/16

N2 - The characteristic of the heat exchange mechanism by slit resonators is numerically investigated. In general, a rocket engine chamber is filled with hot gas, and slit resonators, which are equipped outside of the chamber wall near faceplate, are filled with cold gas. Therefore, when the resonators work well, the cold gas in the resonator might be exchanged for the hot gas in the rocket engine because of acoustic oscillations or vortex generations and motions. In this paper, the heat exchange mechanism by the slit resonators is numerically evaluated on the effect of intensity of incident wave, slit resonator shapes, and kinematic viscosity. In addition, the new idea of a slit resonator shape for the suppression of the heat exchange and its damping performance are mentioned.

AB - The characteristic of the heat exchange mechanism by slit resonators is numerically investigated. In general, a rocket engine chamber is filled with hot gas, and slit resonators, which are equipped outside of the chamber wall near faceplate, are filled with cold gas. Therefore, when the resonators work well, the cold gas in the resonator might be exchanged for the hot gas in the rocket engine because of acoustic oscillations or vortex generations and motions. In this paper, the heat exchange mechanism by the slit resonators is numerically evaluated on the effect of intensity of incident wave, slit resonator shapes, and kinematic viscosity. In addition, the new idea of a slit resonator shape for the suppression of the heat exchange and its damping performance are mentioned.

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M3 - Conference contribution

AN - SCOPUS:84883690024

SN - 9781624102226

T3 - 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference

BT - 49th AIAA/ASME/SAE/ASEE Joint PropulsionConference

T2 - 49th AIAA/ASME/SAE/ASEE Joint PropulsionConference

Y2 - 14 July 2013 through 17 July 2013

ER -

Numerical evaluation of heat exchange mechanism by slit resonators

Abstract

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