Numerical and experimental investigation of trailing edge vortex shedding downstream of a linear turbine cascade

Proceedings of the ASME Turbo Expo

Volumn 1, Issue , 2000, Pages

  Gehrer, A ^a   Lang, H ^a   Mayrhofer, N ^a   Woisetschlager J ^a  

^a GRAZ UNIVERSITY OF TECHNOLOGY   (Austria)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT ENGINES; CASCADES (FLUID MECHANICS); DOPPLER EFFECT; NAVIER STOKES EQUATIONS; SUPERSONIC AIRCRAFT; TURBINES; VORTEX FLOW; VORTEX SHEDDING;

DIRECT DETECTION; EXPERIMENTAL INVESTIGATIONS; IN-DEPTH STUDY; LASER DOPPLER VELOCIMETER (LDV); LINEAR TURBINE CASCADES; NAVIER-STOKES SOLVER; NUMERICAL RESULTS; TRAILING EDGES;

LASER DOPPLER VELOCIMETERS;

EID: 84955064333     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/2000-GT-0434     Document Type: Conference Paper

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