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Keywords: aerodynamic performance
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Journal Articles
Publisher: ASME
Article Type: Research-Article
J. Fluids Eng. June 2024, 146(6): 061202.
Paper No: FE-23-1400
Published Online: February 1, 2024
... a reference for future detailed optimization of this last-stage turbine. 1 Corresponding author. e-mail:  Xiaohua-Liu@sjtu.edu.cn 12 09 2023 14 12 2023 01 02 2024 gas turbine turbine blade redesign aerodynamic performance swept blade National Natural Science...
Journal Articles
Publisher: ASME
Article Type: Research-Article
J. Fluids Eng. August 2022, 144(8): 081501.
Paper No: FE-21-1594
Published Online: March 2, 2022
... in urban areas. The remarkable finding is that the suppression of the flow separation on the blade is an effective way to improve the rotor's aerodynamic performance. As expected, the additional elliptical profile plays a key role in increasing the positive torque and in preventing the flow separation...
Journal Articles
Journal Articles
Publisher: ASME
Article Type: Research-Article
J. Fluids Eng. November 2021, 143(11): 111206.
Paper No: FE-21-1063
Published Online: July 2, 2021
... presented in this study will help in designing new tires with high aerodynamic performance. Conservation of mass (7) ∂ ρ ∂ t + ∇ · ρ V r = 0 Conservation of momentum (8) ∂ ρ ∂ t ρ V r + ∇ · ( ρ V r V ) + ρ ( ω × r...
Journal Articles
Publisher: ASME
Article Type: Research-Article
J. Fluids Eng. October 2020, 142(10): 101204.
Paper No: FE-20-1151
Published Online: June 26, 2020
...Pramod Salunkhe; Yanhua Wu; Hui Tang This work deals with the improvement in aerodynamic performance of a NACA0025 wing model using an array of slotted synthetic jets (SJs). A novel SJ actuator was designed and located at 30% of the chord from the leading edge (LE). Time-resolved particle image...
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Fluids Eng. November 2009, 131(11): 111101.
Published Online: October 19, 2009
...Shun C. Yen; Lung –C. Huang The effects of sweep-back angle ( Λ ) , Reynolds number (Re), and angle of attack ( α ) on the boundary-layer flow structures and aerodynamic performance of a finite swept-back wing were experimentally investigated. The Reynolds number and sweep-back angle used...