Zobrazeno 1 - 7
of 7
pro vyhledávání: '"Qingzhe GAO"'
Publikováno v:
Aerospace, Vol 10, Iss 5, p 398 (2023)
Accurate predictions of the blade response in a multi-row compressor is one of the most important tasks within the design process of compressor blades. Some recent studies have shown that the decoupled method considering only the stator disturbances
Externí odkaz:
https://doaj.org/article/0183ac5f0dc1446cb10d2129a165ce41
Publikováno v:
Entropy, Vol 25, Iss 4, p 613 (2023)
In this paper, the major problems associated with detached eddy simulation (DES) (namely, modeled stress depletion (MSD) and slowing of the RANS to LES transition (RLT)) are discussed and reviewed, and relevant improvements are developed. A modified
Externí odkaz:
https://doaj.org/article/5183aeb8c7714b4f825fb8d2aaccce23
Publikováno v:
Propulsion and Power Research, Vol 9, Iss 1, Pp 26-36 (2020)
Aeroelastic vibration problems are commonly found in modern compressors operating in off-design conditions. Large amplitude vibration could lead to high cycle fatigue (HCF) of blade and usually occurs in front stages of axial compressors. In this stu
Externí odkaz:
https://doaj.org/article/d9d0ad5dc69e45b398b95ed98f483ea5
Publikováno v:
Chinese Journal of Aeronautics. 36:178-190
Publikováno v:
ACM Transactions on Graphics. 41:1-19
Automatic synthesis of realistic co-speech gestures is an increasingly important yet challenging task in artificial embodied agent creation. Previous systems mainly focus on generating gestures in an end-to-end manner, which leads to difficulties in
S-shaped intakes are widely used in aero-engines of modern fighters because of the demand for reducing radar cross-section. Besides, boundary layer ingestion (BLI) configurations are proposed in civil engines recently due to the high propulsion effic
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::44557e699613f9f44c2d7a8391b1dcb0
https://doi.org/10.1115/1.0002426v
https://doi.org/10.1115/1.0002426v
The numerical study is performed by means of an in-house CFD code to investigate the effect of circumferential nonuniform tip clearance due to the casing ovalization on flow field and performance of a turbine stage. A method called fast-moving mesh i
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::f7a3cf3dfd8fe6940a092e364af11e66
https://doi.org/10.1115/1.0002669v
https://doi.org/10.1115/1.0002669v