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pro vyhledávání: '"Vishal Umapathi Choudhari"'
Publikováno v:
Havacılık ve Uzay Teknolojileri Dergisi, Vol 17, Iss 2, Pp 107-121 (2024)
The shock wave boundary layer interaction (SWBLI) due to curved shock is studied prominently, as most military aircrafts and missiles undergo strong SWTBLI due to its curved or blunt shape. These interactions effect the performance of vehicles at sup
Externí odkaz:
https://doaj.org/article/abada65341754532b4b6e061138a0700