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pro vyhledávání: '"Jadhav Akash T."'
Autor:
Jadhav Akash T., Tembhurnikar Payal V., Bhosale Mrunal S., Nandy Jhumki, Sarwar Gulam M.D., Sahoo Devabrata
Publikováno v:
FME Transactions, Vol 52, Iss 3, Pp 419-428 (2024)
To minimize forebody drag in high-speed flying vehicles such as missiles and rockets, contemporary research has focused on computational methods to analyze drag reduction strategies. This study investigates the efficacy of an intermediate aerodisk mo
Externí odkaz:
https://doaj.org/article/973b0b42caf248b5a08160e5ce66cbb5
Publikováno v:
FME Transactions, Vol 48, Iss 4, Pp 779-786 (2020)
Reduction of forebody drag in high speed flying vehicles such as rockets and missiles are of high research interest in the present time. In the present research, drag reduction obtained by using an intermediate aerodisk mounted sharp tip spike has be
Externí odkaz:
https://doaj.org/article/9735f00949f7479cb6b6d52d86e96568