Combustion Instabilities in a Bifurcating Tube: Open- and Closed-Loop Measurements-Reference-Cited by-同舟云学术

Combustion Instabilities in a Bifurcating Tube: Open- and Closed-Loop Measurements

Published:2014-11 Issue:11 Volume:52 Page:2513-2523
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Li Shihuai¹,Zhao Dan¹,Ji Chenzhen¹,Li Junwei²

Affiliation:

1. Division of Aerospace Engineering, Nanyang Technological University, Singapore 639798, Republic of Singapore

2. School of Aerospace Engineering, Beijing Institute of Technology, 100081 Beijing, People’s Republic of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.J052758

Reference36 articles.

1. LieuwenT. C.YangV. (eds.), Combustion Instabilities in Gas Turbine Engines: Operational Experience, Fundamental Mechanisms, and Modeling, Vol. 210, Progress in Astronautics and Aeronautics, AIAA, Reston, VA, 2005, pp. 1–25.

2. Active control of the noise from a rijke tube

3. FEEDBACK CONTROL OF COMBUSTION OSCILLATIONS

4. Model-based control of combustion instabilities

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