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Research Overview on Spike Stall Inception and Slotted Casing Treatment in Aeroengine Compressors [PDF]

open access: goldAerospace
Rotating stall and surge are complex, unsteady flow instability phenomena in aeroengine compressors that pose serious threats to the safety and reliability of both the compressor and the engine as a whole.
Qianfeng Zhang   +2 more
doaj   +2 more sources

Influence of axial spacing on stall development of FBCDZ-10-No20 mode contra-rotating fan

open access: yesMeitan kexue jishu, 2023
The rotating fan is prone to instability such as stall and even surge when operating at low flow rates. In order to study the influence of axial spacings on the stall inception and its development and propagation process of a contra-rotating fan , a ...
Qingguang CHEN   +3 more
doaj   +1 more source

The effect of tip clearance size on pre-stall flow features of a transonic axial compressor by using throttle model

open access: yesAIP Advances, 2023
This paper aims at the numerical analysis of the influence of tip clearance size on the pre-stall flow features of a transonic high-speed compressor by applying the throttle model at the exit of the compressor computational domain.
Khalid Kamal Abdelbagi
doaj   +1 more source

Stall Inception in Low-Pressure Ratio Fans [PDF]

open access: yesJournal of Turbomachinery, 2018
A combined experimental and computational test program, with two low-pressure ratio aero-engine fans, has been used to identify the flow mechanisms at stall inception and the subsequent stall cell growth. The two fans have the same rotor tip clearance, annulus design, and downstream stators, but different levels of tip loading.
Kim, Semi   +5 more
openaire   +2 more sources

Effect of axial spacing on rotating stall performance of FBCDZ-10-No20 contra-rotating fan

open access: yesMeitan kexue jishu, 2023
Mining contra-rotating fan are prone to rotational stall when it operates at low flow rates, which seriously affects the operational stability. The unsteady flow in the full flow passage of a FBCDZ-10-No20 contra-rotating fan at five axial spacings was ...
Qingguang CHEN   +3 more
doaj   +1 more source

Estimations of Compressor Stall and Surge Using Passage Stall Behaviors

open access: yesMachines, 2022
The predictions of the onset of rotating stall and surge are very important in the preliminary design stage of a compressor. Rotating stall and surge are complex instabilities that cause efficiency loss and reduced pressure rise, and, therefore ...
Mohammad Akhlaghi   +2 more
doaj   +1 more source

Origins and Structure of Spike-Type Rotating Stall [PDF]

open access: yes, 2018
In this paper we describe the structures that produce a spiketype route to rotating stall and explain the physical mechanism for their formation. The descriptions and explanations are based on numerical simulations, complemented and corroborated by ...
Day, I. J.   +4 more
core   +4 more sources

Aerodynamic system instability identification with sample entropy algorithm based on feature extraction

open access: yesPropulsion and Power Research, 2023
Based on the sample entropy algorithm in nonlinear dynamics, an improved sample entropy method is proposed in the aerodynamic system instability identification for the stall precursor detection based on the nonlinear feature extraction algorithm in an ...
Mingming Zhang   +5 more
doaj   +1 more source

Axial Flow Compressor Stability Enhancement: Circumferential T-Shape Grooves Performance Investigation

open access: yesAerospace, 2021
This work focuses its attention on possibilities to enhance the stability of an axial compressor using a casing treatment technique. Circumferential grooves machined into the case are considered and their performances evaluated using three-dimensional ...
Marco Porro   +2 more
doaj   +1 more source

Effect of rotor blade tip clearance on aerodynamic performance of high-speed multi-stage axial compressor

open access: yesNihon Kikai Gakkai ronbunshu, 2023
Using a high-speed multistage scale model compressor simulating a middle stage of a gas turbine compressor for power generation, the effects of 3 types of rotor tip clearances on performance and operating range, and the vortex structure of rotor tip ...
Ryosuke SEKI
doaj   +1 more source

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