Two-volume report describes experimental study of flow of air around double-circular-arc turbine blade in cascade of such blades. Provides well-documented, somewhat-complicated flow field used to develop or test future computer codes for simulation of such viscous-flow fields.
Measurements Of Boundary Layers On A Compressor Blade
NASA Tech Briefs ; 15 , 4
1991-04-01
Miscellaneous
No indication
English
Blade Row Interaction Effects on Compressor Measurements
Online Contents | 1993
|Blade row interaction effects on compressor measurements
AIAA | 1993
|Emerald Group Publishing | 1999