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pro vyhledávání: '"Patil Manthan"'
Autor:
Patil Manthan, Gawade Rajesh, Potdar Shubham, Nadaf Khushabu, Suresh Sanoj P., Sahoo Devabrata
Publikováno v:
FME Transactions, Vol 49, Iss 2, Pp 395-400 (2021)
Flow over a conventional delta wing has been studied experimentally at a subsonic flow of 20 m/sec and the flow field developed at higher angle of attack varying from 10° to 20° has been captured. A vortex generator is mounted on the leeward surfac
Externí odkaz:
https://doaj.org/article/6de8e69861144dca83fcc0017d667732
