The influence of technical surface roughness caused by precision forging on the flow around a highly loaded compressor cascade

Journal of Turbomachinery

Volumn 122, Issue 3, 2000, Pages 416-425

  Leipold, R ^a   Boese, M ^a   Fottner, L ^a  

^a BUNDESWEHR UNIVERSITY MUNICH   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC LOADS; ANEMOMETERS; BOUNDARY LAYER FLOW; CASCADES (FLUID MECHANICS); COPPER; FORGING; PRESSURE DISTRIBUTION; REYNOLDS NUMBER; SURFACE ROUGHNESS; TURBOMACHINE BLADES; WIND TUNNELS;

HIGHLY LOADED COMPRESSOR CASCADE; PRECISION FORGING; SEPARATION BUBBLE;

COMPRESSORS;

CASCADE; COMPRESSOR SYSTEM; FLOW AROUND OBJECT; FORGING; SURFACE ROUGHNESS;

EID: 0034233043     PISSN: 0889504X     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.1302286     Document Type: Conference Paper

References (15)

1. The effect of adding roughness and thickness to a transonic axial compressor rotor
2. Measurements of the boundary layer development along a turbine blade with rough surfaces
3. The high speed cascade wind tunnel of the German Armed Forces University Munich
4. A measurement technique to investigate the influence of surface roughness on the flow around a highly loaded compressor cascade
5. Experimentelle und theoretische Untersuchung der wesentlichen Einflussfaktoren auf die Spalt- und Sekundarstromung in Verdichtergittern
6. Entwicklung des Laser-Zwei-Fokus-Verfahrens fur die beruhrungslose Messung der Stromungsvektoren, insbesondere in Turbomaschinen