Effects of Trumpet on the Flow Characteristics of Pressure Swirl Injectors
Author:
Affiliation:
1. China Aerodynamics Research and Development Center, 621000 Mianyang, People’s Republic of China
2. National University of Defense Technology, 410073 Changsha, People’s Republic of China
Funder
Chinese Program for New Century Excellent Talents in University
National Basic Research Program of China
National Natural Science Foundation of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.B36408
Reference35 articles.
1. Effect of geometric parameters on the spray cone angle in the pressure swirl injector
2. Effect of Geometric Parameters on Simplex Atomizer Performance
3. Droplet size distribution and evaporation characteristics of fuel spray by a swirl type atomizer
4. An experimental study on fuel spray-induced vortex-like structures
5. Effect of viscosities on structure and instability of sprays from a swirl atomizer
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