Tag Archives: Air-launched Missile

Heat Transfer Characteristics of the Missile Radome Considering Flight Scenario

1.Events, High-Speed Aerodynamics and Aerothermodynamics, HiSST 2024By Beata Wierzbińska-Prus May 10, 2024

Sangbin HAN, Hyung Mo BAE, Jihyuk KIM, Dongkyun LEE, Kyeongho LEE, Sunghwan YIM, Hyung Hee CHO

DOI Number: XXX-YYY-ZZZ

Conference number: HiSST 2024 – 0057