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Autor:
Murat Gecgel, Yavuz Nacaklı
Publikováno v:
Havacılık ve Uzay Teknolojileri Dergisi, Vol 11, Iss 2, Pp 71-82 (2018)
This study presents the outcomes of a series of computational fluid dynamics analyses conducted to obtain unsteady solutions of the flowfields around single rotor helicopter configurations. We use a methodology to obtain the time dependent solutions
Externí odkaz:
https://doaj.org/article/15cf4ec4a7d74b2d9ff21aaf05569660