The Effect of Adding Roughness and Thickness to a Transonic Axial Compressor Rotor,’’

Authors
Publication date
1 January 1995
Publisher

Abstract

The performance deterioration of a high-speed axial compressor rotor due to surface roughness and airfoil thickness variations is reported. A 0.025 mm (0.001 in.

    Similar works

    Full text

    thumbnail-image

    Available Versions

    CiteSeerX

    redirect
    oaioai:CiteSeerX.psu:10.1.1.1055....
    Last time updated on 07/12/2020