A simultaneous use of a leading-edge fillet and a non-axisymmetrically contoured endwall in a turbine stage-Reference-Cited by-同舟云学术

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A simultaneous use of a leading-edge fillet and a non-axisymmetrically contoured endwall in a turbine stage

Published:2021-11 Issue: Volume:118 Page:106985
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Turgut Özhan H.^ORCID,Camci Cengiz^ORCID

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference32 articles.

1. Predictions of endwall losses and secondary flows in axial flow turbine cascades;Sharma;J. Turbomach.,1987

2. Loss mechanisms in turbomachines;Denton;J. Turbomach.,1993

3. Reduction of secondary flow losses in turbine cascades by leading edge modifications at the endwall;Sauer;J. Turbomach.,2001

4. Computational design and experimental evaluation of using a leading edge fillet on a gas turbine vane;Zess;J. Turbomach.,2002

5. Controlling secondary-flow structure by leading-edge airfoil fillet and inlet swirl to reduce aerodynamic loss and surface heat transfer;Shih;J. Turbomach.,2003

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1. Performance Enhancement of Hydraulic Axial Turbine Rotor Using Enclosure at Upstream and Downstream Side;Journal of Energy Engineering;2024-10

2. Influence of a novel leading-edge winglet on the aerodynamic characteristics of a highly loaded turbine;Aerospace Science and Technology;2024-09

3. Unsteady Interaction Between Purge Flow and Secondary Flow in High-Lift Low-Pressure Turbine;Journal of Turbomachinery;2024-06-07

4. Experimental investigation on the aerodynamic performance of a transonic turbine rotor with non-axisymmetric endwall;Aerospace Science and Technology;2024-04

5. Experimental test of a compressor cascade with non-axisymmetric end-wall contouring at off-design conditions;Applied Thermal Engineering;2024-03

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