Effects of casing treatment on behavior of tip leakage flow in an isolated axial compressor rotor blade row

Author： Taghavi-Zenouz Reza   Eslami Siamak  

Publisher： Taylor & Francis Ltd

ISSN： 0253-3839

Source： Journal of the Chinese Institute of Engineers, Vol.36, Iss.7, 2013-10, pp. : 819-830

Disclaimer: Any content in publications that violate the sovereignty, the constitution or regulations of the PRC is not accepted or approved by CNPIEC.

Previous Menu Next

Abstract

Related content

Effect of turbine inlet temperature on rotor blade tip leakage flow and heat transfer

By Kim Sung In   Rahman Md Hamidur   Hassan Ibrahim  

International Journal of Numerical Methods for Heat & Fluid Flow, Vol. 22, Iss. 1, 2012-01 ,pp. : 73-93

Emerald Group Publishing Ltd

Access to resources Recommend Favorite

Full Annulus Simulations of a Transonic Axial Compressor Stage with Distorted Inflow at Transonic and Subsonic Blade Tip Speed †

By Haug Jakob P.   Niehuis Reinhard  

International Journal of Turbomachinery, Propulsion and Power, Vol. 3, Iss. 1, 2018-02 ,pp. : 7-7

MDPI

Access to resources Recommend Favorite

Effects of rotor blade-tip geometry on helicopter trim and control response

By  

The Aeronautical Journal, Vol. 121, Iss. 1239, 2017-05 ,pp. : 637-659

Cambridge University Press

Access to resources Recommend Favorite

Hovering rotor computations using an aeroelastic blade model

By  

The Aeronautical Journal, Vol. 116, Iss. 1180, 2012-06 ,pp. : 621-649

Cambridge University Press

Access to resources Recommend Favorite

Lagrangian formulation for the rapid estimation of helicopter rotor blade vibration characteristics

By  

The Aeronautical Journal, Vol. 118, Iss. 1206, 2014-08 ,pp. : 861-901

Cambridge University Press

Access to resources Recommend Favorite