TY - GEN
T1 - Flow measurements in a first stage nozzle cascade having leakage and assembly features
T2 - 2005 ASME International Mechanical Engineering Congress and Exposition, IMECE 2005
AU - Piggush, J. D.
AU - Simon, T. W.
PY - 2005/12/1
Y1 - 2005/12/1
N2 - This work supports new gas turbine designs for improved performance by evaluating endwall leakage and assembly features in a cascade that is representative of a first stage stator passage. The present paper documents component misalignment and leakage flow effects on the aerodynamic losses within a passage having one contoured and one straight endwall. Steps on the endwall and leakage flows through the endwall can lead to thicker endwall boundary layers, stronger secondary flows and possibly additional vortex structures in the passage. The paper compares losses with steps of various geometries and leakage of various flow rates to assess their importance on aerodynamic losses in this contoured passage. In particular, features associated with the conibustor-to-turbine transition piece and the slash-face gap, a gap between two vane segments on the vane platform, are addressed.
AB - This work supports new gas turbine designs for improved performance by evaluating endwall leakage and assembly features in a cascade that is representative of a first stage stator passage. The present paper documents component misalignment and leakage flow effects on the aerodynamic losses within a passage having one contoured and one straight endwall. Steps on the endwall and leakage flows through the endwall can lead to thicker endwall boundary layers, stronger secondary flows and possibly additional vortex structures in the passage. The paper compares losses with steps of various geometries and leakage of various flow rates to assess their importance on aerodynamic losses in this contoured passage. In particular, features associated with the conibustor-to-turbine transition piece and the slash-face gap, a gap between two vane segments on the vane platform, are addressed.
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U2 - 10.1115/IMECE2005-83032
DO - 10.1115/IMECE2005-83032
M3 - Conference contribution
AN - SCOPUS:33645660412
SN - 0791842215
SN - 9780791842218
T3 - American Society of Mechanical Engineers, Heat Transfer Division, (Publication) HTD
SP - 525
EP - 534
BT - Proceedings of the ASME Heat Transfer Division 2005
Y2 - 5 November 2005 through 11 November 2005
ER -