Principles of non-intrusive diagnostic techniques and their applications for fundamental studies of combustion instabilities in gas turbine combustors: A brief review-Reference-Cited by-同舟云学术

Principles of non-intrusive diagnostic techniques and their applications for fundamental studies of combustion instabilities in gas turbine combustors: A brief review

Published:2019-01 Issue: Volume:84 Page:585-603
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Ruan Can,Chen Feier,Cai Weiwei,Qian Yong^ORCID,Yu Liang,Lu Xingcai

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference157 articles.

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3. Thermo-acoustic velocity coupling in a swirl stabilized gas turbine model combustor;Caux-Brisebois;Combust. Flame,2014

4. Effect of fuel–air mixture velocity on combustion instability of a model gas turbine combustor;Yoon;Appl. Therm. Eng.,2013

5. Simultaneous OH-PLIF and PIV measurements in a gas turbine model combustor;Sadanandan;Appl. Phys. B,2008

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