Results 31 to 40 of about 18,174 (265)
Flow Field Diagnosis in Multistage Axial Compressors [PDF]
Volume 1: Turbomachinery, 1996 A mathematical model is developed for the flow field diagnosis problem in multistage axial compressors. In view of the ill-posedness of the diagnostic problem, an effective measure is adopted to transfer the diagnostic problem into a variational problem which is solved by a regularization method. Two numerical results demonstrate the rationality of the
Zhen Zhang, Dajun Ye, Jing Liu
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Inter-Stage Dynamic Performance of an Axial Compressor of a Twin-Shaft Industrial Gas Turbine
Machines, 2020 In this study, the inter-stage dynamic performance of a multistage axial compressor is simulated through a semi-empirical model constructed in the Matlab Simulink environment.
Samuel Cruz-Manzo +3 more
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Aerospace, 2021 Helicopters often operate in dusty sites, ingesting huge amounts of contaminants during landing, take-off, hover-taxi, and ground operations. In specific locations, the downwash of the rotor may spread soil particles from the ground into the environment ...
Alessandro Vulpio +3 more
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Авіаційно-космічна техніка та технологія, 2019 Gas Turbine Engine (GTE) operating characteristics such as thrust (or power), specific fuel consumption and other cycle parameters on different regimes, can be determined by engine modeling and applying correspondent calculation method.
Людмила Георгиевна Бойко +2 more
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TO THE OPTIMUM DESIGN OF THE AXIAL MULTI-STAGE COMPRESSOR
Авіаційно-космічна техніка та технологія, 2017 The work is devoted to the development of an integrated approach to the aerodynamic improvement of the blade vanes of multistage axial compressors of gas turbine engines.
Владимир Петрович Герасименко +1 more
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International Journal of Aerospace Engineering, 2021 A new design optimization method is proposed for the problem of high-precision aerodynamic design of multistage axial compressors. The method mainly contains three aspects: full-blade surface parametrization can significantly reduce the number of control
Jinxin Cheng +3 more
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An Investigation of Spanwise Mixing in Multistage Axial Flow Compressors [PDF]
Volume 1: Turbomachinery, 1992 An equation system has been deduced for meridional throughflow fields of multistage axial flow compressors, presenting different kinds of spanwise mixing effects of the fields in a unified form. The spanwise mixing in compressors is caused by three kinds of effects, molecular motion, turbulent diffusion, and circumferential non–uniformities, the last ...
S.-M. Li, M.-Z. Chen
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Machines, 2023 A four-blade-passage numerical model was developed for a two-stage axial-flow compressor with an inlet guide vane (IGV) for the purpose of studying the steady and dynamic characteristics of the compressor approaching its stability limit.
Tong Wang, Xiangyuan Dou, Yongwen Liu
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Aerodynamic design and numerical simulation of mixed-axial flow multi-stage compressor
Zhongguo Jianchuan Yanjiu, 2018 [Objectives] The performance of a gas turbine engine can be determined by the performance of the compressor. As one of the core components of a gas turbine engine,the design of the compressor is of critical importance in the design of the engine overall.[
ZHANG Xiaoyang +3 more
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Effect and Mechanism of Roughness on the Performance of a Five-Stage Axial Flow Compressor
Aerospace, 2022 In order to prolong the service life of multistage axial compressors, it is increasingly important to study the influence of blade surface roughness on the compressor performance.
Yan Chen, Chunxiang Gao, Wuli Chu
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