Numerical investigation of typical valveless pulse combustor working process

被引:0
|
作者
Zhang Tao [1 ]
Zhan Yong [2 ]
Cai Wenxiang [2 ]
机构
[1] Beihang Univ, Beijing 100083, Peoples R China
[2] Nanjing Univ Sci & Technol, Nanjing 210094, Jiangsu, Peoples R China
基金
中国国家自然科学基金;
关键词
valveless pulse jet; numerical simulation; multi-cycle component; pulse combsution;
D O I
10.1016/j.egypro.2017.11.107
中图分类号
TE [石油、天然气工业]; TK [能源与动力工程];
学科分类号
0807 ; 0820 ;
摘要
Due to the valveless pulse combustor's simplicity in structure and reliability in performance, it may be the most ideal low cost high efficient combustion system for agriclutural energy. In a typical valveless pulse combustion, a numerical simulation is performed to understand the variation of flow field and to research the performance of the valveless pulse combustor by use of general CFD simulation software (CFX). Results of numerical simulation indicate that the pulse combustor works felicitously and working process of the pulse combustor is consistent with the basic theory of the pulse combustion. (C) 2017 The Authors. Published by Elsevier Ltd.
引用
收藏
页码:287 / 291
页数:5
相关论文
共 50 条
  • [31] Experimental Research on Operational Characteristics of a Helmholtz-type Valveless Self-excited Pulse Combustor
    Xu, Yanying
    Zhai, Ming
    Dong, Peng
    Wang, Fei
    2011 ASIA-PACIFIC POWER AND ENERGY ENGINEERING CONFERENCE (APPEEC), 2011,
  • [32] Isolation of back pressure waves in a valveless pulse detonation combustor with inlet air of high total temperature
    Jie, Lu
    Hao, Zhang
    Wenhao, Tan
    Longxi, Zheng
    FUEL, 2023, 331
  • [33] Numerical Investigation on the Effect of Inflow Mach Numbers on the Combustion Characteristics of a Typical Cavity-Based Supersonic Combustor
    Bordoloi, Namrata
    Pandey, Krishna Murari
    Sharma, Kaushal Kumar
    MATHEMATICAL PROBLEMS IN ENGINEERING, 2021, 2021
  • [34] Numerical investigation on a typical scramjet combustor using cavity floor H2 fuel injection strategy
    Choubey, Gautam
    Solanki, Malhar
    Bhatt, Tathya
    Kshitij, G.
    Yuvarajan, D.
    Huang, Wei
    ACTA ASTRONAUTICA, 2023, 202 : 373 - 385
  • [35] Numerical Investigation on the Cold Flow Field of a Typical Cavity-based Scramjet Combustor with Double Ramp Entry
    Periyasamy, S.
    Ragul, S.
    Sundararaj, K.
    Premkumar, P. S.
    INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES, 2022, 39 (03) : 439 - 449
  • [36] Experimental investigation of air-breathing valveless pulse detonation engine
    School of Power and Energy, Northwestern Polytechnical University, Xi'an 710072, China
    Shiyan Liuti Lixue, 2007, 1 (87-92):
  • [37] Numerical Investigation on detonation combustion waves of hydrogen-air mixture in pulse detonation combustor with blockage
    Debnath, Pinku
    Pandey, K. M.
    ADVANCES IN AIRCRAFT AND SPACECRAFT SCIENCE, 2023, 10 (03): : 203 - 222
  • [38] Numerical simulation investigation on a hydrogen micromix Combustor
    Mo D.
    Shang S.
    Lin Y.
    Ma H.
    Liu Y.
    Hangkong Dongli Xuebao/Journal of Aerospace Power, 2023, 38 (11): : 2701 - 2710
  • [39] Numerical Simulations of a Typical Hydrogen Fueled Scramjet Combustor with a Cavity Flameholder
    Huang, Wei
    Luo, Shi-bin
    Pourkashanian, Mohamed
    Ma, Lin
    Ingham, Derek B.
    Liu, Jun
    Wang, Zhen-guo
    WORLD CONGRESS ON ENGINEERING, WCE 2010, VOL II, 2010, : 1000 - 1003
  • [40] NUMERICAL STUDY OF HYDROGEN AIR MIXING FLOWFIELD IN A TYPICAL COMBUSTOR GEOMETRY
    TRINH, HP
    ISAAC, KM
    CHEN, YS
    INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 1989, 14 (10) : 737 - 748