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Авіаційно-космічна техніка та технологія, 2022 When creating a modern aircraft, the principle of optimal integration of the power plant and the aircraft is used to ensure the maximum target function, determined by its functional purpose.
Oleg Zhornik +3 more
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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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Effects of Configuration and Slot Angle of the Bleed System on the Performance of Hypersonic Inlet
气体物理, 2023 The numerical simulation of a typical two-dimensional hypersonic inlet was carried out to study the effects of configuration and slot angle of the bleed system on the performance of hypersonic inlet.
Hao-Yu CHEN, He-Xia HUANG, Hui-Jun TAN
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Aerodynamic Studies in the Static Components of A Centrifugal Compressor Stage Authors [PDF]
Journal of Mechanical Engineering and Sciences, 2011 Aerodynamic studies in the static components of a centrifugal compressor stage were conducted using the computational fluid dynamics solver FLUENT. For the simulation study, a typical centrifugal compressor stage geometry with a flow coefficient of 0 ...
K. Srinivasa Reddy +2 more
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Study on Three-Dimensional Inner Flow Field Characteristics and Performance of Scramjet [PDF]
MATEC Web of Conferences, 2019 The three-dimensional characteristics and performance of the flow field in the inlet of the scramjet engine were numerically simulated by CFD software. The flow characteristics in the width direction of the inlet and the influence of the aspect ratio on ...
Gao Feng, Zhao Jie, Zhang Cheng Tao
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Hangkong gongcheng jinzhan, 2020 The accelerating effect, viscous effect, and rotating effect of the propeller slipstream are of significant influences on the performance of the inlet.
WANG Limin, ZHANG Yanjun
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Numerical Study on Internal flow Field Dynamic Performance of Scramjet [PDF]
MATEC Web of Conferences, 2019 The pressure pulsation caused by the combustion of the combustion chamber of the scramjet engine has a great influence on the flow and performance of the inlet.
Gao Feng, Zhao Jie, Chen Feng Li
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Study on Aerodynamic Design of the Front Auxiliary Inlet
Aerospace, 2023 Submerged inlets have been widely used in advanced aircraft due to their excellent stealth characteristics, but they also suffer from poor aerodynamic performance.
Junyao Zhang, Hao Zhan, Baigang Mi
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Influence of Propeller Slipstream on the Flow Field of S-Shaped Intake
International Journal of Aerospace Engineering, 2021 For turboprop engine, the S-shaped intake affects the engine performance and the propeller is not far in front of the inlet of the S-shaped intake, so the slipstream inevitably affects the flow field in the S-shaped intake and the engine performance ...
Shuili Ren, Peiqing Liu
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Numerical Study on Effects of High-Frequency Arrayed Energy Deposition on Scramjet Combustor Performance [PDF]
Hangkong bingqi, 2023 For the supersonic flows have large momentum, it is difficult to get higher penetration depth because of the influence of transverse jet on incoming flow so as to affect the mixing and combustion efficiency of jet in scramjet combustor.
Cai Zilin, Gao Feng, Wang Hongyu, Ma Cenrui
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