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Effects of self-pulsation on the spray characteristics of gas–liquid swirl coaxial injector

  • Published:2016-10 Issue: Volume:127 Page:249-259
  • ISSN:0094-5765
  • Container-title:Acta Astronautica
  • language:en
  • Short-container-title:Acta Astronautica

Author:

Kang Zhongtao,Li Qinglian,Cheng Peng,Zhang Xinqiao,Wang Zhen-guo

Funder

Chinese Program for New Century Excellent Talents in University

National Natural Science Foundation of China

National Basic Research Program of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference34 articles.

1. Rocketry mentors, rocketry practitioners and unique space pioneers;Lundquist;Acta Astronaut.,2015

2. Lagrangian modelling of turbulent spray combustion under liquid rocket engine conditions;Gomet;Acta Astronaut.,2014

3. Numerical study of liquid propellants combustion for space applications;Amri;Acta Astronaut.,2011

4. A feasibility study on using inkjet technology, micropumps, and MEMs as fuel injectors for bipropellant rocket engines;Glynne Jones;Acta Astronaut.,2010

5. The flowrate characteristics of gas–liquid coaxial swirling and unswirling injectors;Zhou;J. Natl. Univ. Def. Technol.,1999
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