Results 21 to 30 of about 5,605 (299)
Analysis of Flow Field Distortion in Ship Inlet System and Its Effect on Compressor Performance [PDF]
Journal of Applied Fluid Mechanics, 2023 Intake system structure design is categorized under gas turbine marine technology, and its performance affects the inlet flow field of the compressor, thereby impacting the overall operation stability of the gas turbine.
Z. Y. Wang, C. X. He, Y. L. Qu
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Applied Sciences, 2023 Submerged inlet has been widely used in UAVs and cruise missiles due to its good stealth characteristics, but it also brings the disadvantage of poor aerodynamic characteristics.
Junyao Zhang, Baigang Mi
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Aerospace, 2023 The submerged inlet exhibits good stealth characteristics and lower drag, but it has a low total pressure recovery coefficient and high distortion rate, which limits its widespread application. This paper proposes a vortex diverter aimed at enhancing the
Junyao Zhang, Hao Zhan, Baigang Mi
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Development of a Method for Enhanced Fan Representation in Gas Turbine Modeling [PDF]
, 2011 A challenge in civil aviation future propulsion systems is expected to be the integration with the airframe, coming as a result of increasing bypass ratio or above wing installations for noise mitigation. The resulting highly distorted inlet flows to the
Anestis Kalfas +7 more
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The effect of upstream duct boundary layer growth and compressor blade lean angle variation on an axial compressor performance [PDF]
, 2010 The compressor of a gas turbine engine is extremely vulnerable on upstream duct- induced flow non-uniformities whether the duct is an engine intake or an interconnecting duct.
Templalexis, I. +3 more
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AIP Advances, 2023 In order to increase the stalling margin of a compressor under different inlet conditions, especially under inlet distortion conditions, a new coupled casing processing structure is proposed in this paper.
Hong Xie +3 more
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Experimental and Numerical Analysis of a Compressor Stage under Flow Distortion
International Journal of Turbomachinery, Propulsion and Power, 2021 On many occasions, fan or compressor stages have to face azimuthal flow distortion at inlet, which affects their performance and stability. These flow distortions can be caused by external events or by some particular geometrical features.
Alberto Baretter +6 more
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Simulation Research on Influence of Inlets Crossing Position on Solid Ducted Rocket Performance [PDF]
Hangkong bingqi, 2021 A 3D combustion simulation research about the varied inlets crossing positions of the solid ducted rocket with two inlets is carried out to study the influence of inlets crossing position on the performance of solid ducted rocket with fixed primary fuel ...
Li Dong, Qiu Zhen’an, Wang Feng, Zhang Hongfei, Guo Yinhao
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Energies, 2021 In this paper, an experimental study was carried out on the rotating instability in an axial compressor subjected to inlet steady paired swirl distortion.
Rong Xu +4 more
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Inlet Flow Distortions in Centrifugal Fans [PDF]
1984 Joint Power Generation Conference: GT Papers, 1984 Recent measurements of the performance of a centrifugal fan subjected to inlet flow distortion are presented. Results of axial and multilobed distortion modes are discussed in the context of a previously published study to provide a more comprehensive evaluation of related fan performance degradation.
S. Madhavan, J. DiRe, T. Wright
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