Numerical Investigation on Flow Separation Control of Low Reynolds Number Sinusoidal Aerofoils

The paper presents a computational analysis of the characteristics of a NACA 634-021 aerofoil incorporated with sinusoidal leading-edge protuberances at Re = 14,000. The protuberances are characterized by an amplitude and wavelength of 12% and 50% of the aerofoil chord length respectively. An unstea...

Бүрэн тодорхойлолт

Номзүйн дэлгэрэнгүй
Үндсэн зохиолчид: Joy, Jesline, Ibrahim, Imran H., New, Tze How
Бусад зохиолчид: School of Mechanical and Aerospace Engineering
Формат: Conference Paper
Хэл сонгох:English
Хэвлэсэн: 2017
Нөхцлүүд:
Онлайн хандалт:https://hdl.handle.net/10356/83344
http://hdl.handle.net/10220/42539