Transactions of Nanjing University of Aeronautics & Astronautics
Archive > Volume 36 Issue 5 > 2019,36(5):828-837. DOI:10.16356/j.1005-1120.2019.05.014 Prev Next

Effect of Swirl Preset Vorticity on Combustion Performance of Lobe Nozzle Combustor Chamber

CHINA AERO-SCIENCES

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