Zobrazeno 1 - 10
of 13
pro vyhledávání: '"Kailong Xia"'
Publikováno v:
Aerospace, Vol 10, Iss 3, p 226 (2023)
The moving endwall has a great influence on the development and stability of axial compressor leakage flow. This paper presents a novel experimental facility with a high-speed moving endwall for studying axial compressor leakage flow. The uniqueness
Externí odkaz:
https://doaj.org/article/dc9162f64cba421499a8392e6f7b3c2c
Publikováno v:
Journal of the Global Power and Propulsion Society. 7:113-126
The hub and casing walls of axial compressors are often modeled as smooth continuous surfaces in CFD simulations, but in real geometries, non-smooth pinches, steps and leakage cavities may exist. In the GPPS first Turbomachinery CFD Workshop, a compr
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ebf6cc63001814e3186f9a238d9a7aa0
https://doi.org/10.33737/jgpps/161708
https://doi.org/10.33737/jgpps/161708
Publikováno v:
Journal of the Global Power and Propulsion Society. 7:13-29
This paper presents a comprehensive validation and verification study of turbomachinery Reynolds-averaged Navier-Stokes flow solvers on the transonic axial compressor TUDa-GLR-OpenStage. Two commercial solvers namely Ansys CFX and Numeca FineTurbo ar
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::38932dc12bc1e07295f83f2209746451
https://doi.org/10.33737/jgpps/158034
https://doi.org/10.33737/jgpps/158034
Publikováno v:
Aerospace Systems. 6:107-118
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c356fa3657b142f8ee72527e186d11f5
https://doi.org/10.1007/s42401-022-00173-7
https://doi.org/10.1007/s42401-022-00173-7
Publikováno v:
Journal of Shanghai Jiaotong University (Science).
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d5aeb0b6ab335002e63ff8d7778c7f8c
https://doi.org/10.1007/s12204-022-2541-3
https://doi.org/10.1007/s12204-022-2541-3
Publikováno v:
Volume 10A: Turbomachinery — Axial Flow Fan and Compressor Aerodynamics.
An axial single-stage high-speed test rig was numerically studied in this paper with half-annulus URANS simulations to describe the flow characteristics at the near stall condition. Numerical probes were arranged circumferentially near the casing in
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::018f2b7522e979b415f8df0d95f1c977
https://doi.org/10.1115/gt2022-82366
https://doi.org/10.1115/gt2022-82366
Publikováno v:
Volume 10A: Turbomachinery — Axial Flow Fan and Compressor Aerodynamics.
The cavity flow of shrouded stators is quite complex and not yet completely understood, especially for its loss characteristics. In this paper, a matrix of numerical simulations was designed and conducted to investigate the loss characteristics of th
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::feb8d47913a16ab0de42222593cba9d3
https://doi.org/10.1115/gt2022-82361
https://doi.org/10.1115/gt2022-82361
Publikováno v:
International Journal of Turbo & Jet-Engines; May2024, Vol. 41 Issue 2, p363-375, 13p
Publikováno v:
Journal of Aerospace Engineering; Sep2023, Vol. 36 Issue 5, p1-16, 16p
Publikováno v:
Physics of Fluids; Aug2023, Vol. 35 Issue 8, p1-17, 17p