Simulation investigation on flow and combustion characteristics in a high temperature rise combustor based on RQL under different primary holes spacing-Reference-Cited by-同舟云学术

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Simulation investigation on flow and combustion characteristics in a high temperature rise combustor based on RQL under different primary holes spacing

Published:2021-11-10 Issue:12 Volume:43 Page:
ISSN:1678-5878
Container-title:Journal of the Brazilian Society of Mechanical Sciences and Engineering
language:en
Short-container-title:J Braz. Soc. Mech. Sci. Eng.

Author:

Chen Jian^ORCID,Li Jianzhong,Hu Ge,Dong Qingqing

Funder

Natural Science Foundation of Guizhou Province

Publisher

Springer Science and Business Media LLC

Subject

Mechanical Engineering,General Engineering,Aerospace Engineering,Automotive Engineering,Industrial and Manufacturing Engineering,Applied Mathematics

Link

https://link.springer.com/content/pdf/10.1007/s40430-021-03250-8.pdf

Reference31 articles.

1. Mongia H (2011) Engineering aspects of complex gas turbine combustion mixers part I: high ΔT. In: 49th AIAA aerospace science meeting including the new horizons forum and aerospace exposition, Orlando, Florida

2. Mongia H (2011) Engineering aspects of complex gas turbine combustion mixers part II: high T3. In: 49th AIAA aerospace science meeting including the new horizons forum and aerospace exposition, Orlando, Florida

3. Mongia H (2011) Engineering aspects of complex gas turbine combustion mixers part III: 30 OPR. In: 9th annual international energy conversion engineering conference, San Diego, California

4. Bahr DW (1987) Technology for the design of high temperature rise combustors. J Propul Power 3(2):179–186

5. Mongia H (1997) Gas turbine combustion design, technology and research—current status and future direction. In: 33rd AIAA/ASME/ASEE joint propulsion conference and exhibit, Seattle, WA

Cited by 3 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Simulation study on the flow characteristic and combustion performance in a high-temperature rise combustor based on RQL under different length of quench zone;Journal of the Brazilian Society of Mechanical Sciences and Engineering;2024-05-26

2. Influence of primary jets on the combustion performance of a rich quench lean combustor: A numerical and experimental investigation;Aerospace Science and Technology;2024-05

3. Effect of Primary Holes Structure on Flow Characteristic and Combustion Performance of High Temperature Rise Combustor Based on RQL;International Journal of Aeronautical and Space Sciences;2022-12-25

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