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An Improved Integral Method for Prediction of Distorted Inlet Flow Propagation in Axial Compressor

An improved integral method is proposed and developed for the quantitative prediction of distorted inlet flow propagation through axial compressor. The novel integral method is formulated using more appropriate and practical airfoil characteristics, with less assumptions needed for derivation. The r...

Бүрэн тодорхойлолт

-д хадгалсан:
Номзүйн дэлгэрэнгүй
Үндсэн зохиолчид: Eddie Yin-Kwee Ng, Ningyu Liu, Hong Ngiap Lim, Daniel Tan
Формат: Artigo
Хэл сонгох:Inglês
Хэвлэсэн: Wiley 2005-01-01
Цуврал:International Journal of Rotating Machinery
Нөхцлүүд:
Онлайн хандалт:http://dx.doi.org/10.1155/IJRM.2005.117
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