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Date of Publication:2024-12-03
Journal:宇航学报
Volume:45
Issue:10
Page Number:1509-1523
ISSN No.:1000-1328
Key Words:Ablation model; Airflow erosion; Flight vehicle; Mechanical denudation; Thermal protection material
CN No.:11-2053/V
Next One:Experimental research on bidirectional vortices in cold wall rocket thruster
