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Engine performance analysis and optimization of a dual-mode scramjet with varied inlet conditions
Authors:Lu Tian  Li-Hong Chen  Qiang Chen  Feng-Quan Zhong  Xin-Yu Chang
Affiliation:State Key Laboratory of High-Temperature Gas Dynamics, Institute of Mechanics, Chinese Academy of Sciences, Beijing 100190, China
Abstract:
Keywords:Dual-mode scramjet  Engine performance  Thrust  Optimization  Heat release distribution  Simulated annealing algorithm
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