Zobrazeno 1 - 10
of 15
pro vyhledávání: '"Jong-Shang Liu"'
Publikováno v:
Volume 2B: Turbomachinery.
Typical turbine blade design systems are based on parametric studies and engineering experience. Best practices use feedback from manufactured hardware to additionally create producible designs and establish tolerances. Often there is a large gap in
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::519ef66d9a7baa41f2a3ef797209b59c
https://doi.org/10.1115/gt2018-75536
https://doi.org/10.1115/gt2018-75536
Publikováno v:
Volume 5A: Heat Transfer.
In order to have higher power to weight ratio and higher efficiency gas turbine engines, turbine inlet temperatures continue to rise. State-of-the-art turbine inlet temperatures now exceed the turbine rotor material capability. Accordingly, one of th
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::91365cd2bbc4772cacb859c50de97675
https://doi.org/10.1115/gt2017-64596
https://doi.org/10.1115/gt2017-64596
Autor:
Riccardo Bozzola, Jong-Shang Liu
Publikováno v:
AIAA Journal. 31:2068-2074
A three-dimensional viscous flow code was used to study the tip clearance flow in linear turbine cascades. Two test cases with detailed measurements were used for validation. The flow properties inside the tip gap, such as static pressure, velocity,
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::cb8fd871d2a6a618be643b989052a86c
https://doi.org/10.2514/3.49123
https://doi.org/10.2514/3.49123
Publikováno v:
38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::923f8ab74c7aaff755cc783a3372681b
https://doi.org/10.2514/6.2002-3646
https://doi.org/10.2514/6.2002-3646
Publikováno v:
35th Joint Propulsion Conference and Exhibit.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5fb0959d3a5d6e02ef9c37f1ffdeb193
https://doi.org/10.2514/6.1999-2382
https://doi.org/10.2514/6.1999-2382
Autor:
Durbha V. Murthy, Jong-Shang Liu
Publikováno v:
Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery.
The flutter analysis capability of the quasi-3D aeroelastic computational fluid dynamic (CFD) code UNSFLO is evaluated by comparing to unsteady pressure results in an oscillating cascade. The geometry is two-dimensional and the oscillation is well-co
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::48bd0734811a75c8a80beb6cf981f43f
https://doi.org/10.1115/99-gt-022
https://doi.org/10.1115/99-gt-022
Publikováno v:
30th Joint Propulsion Conference and Exhibit.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c1e53eb50215b4e2a69c324f5ec65121
https://doi.org/10.2514/6.1994-2928
https://doi.org/10.2514/6.1994-2928
Autor:
Riccardo Bozzola, Jong-Shang Liu
Publikováno v:
31st Aerospace Sciences Meeting.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ad85211396396c2f64bd52482c1d46e6
https://doi.org/10.2514/6.1993-391
https://doi.org/10.2514/6.1993-391
Publikováno v:
Volume 1: Turbomachinery.
Analytical and experimental investigations were conducted to study important tip clearance flow phenomena, such as leakage vortex, flow underturning, and the effect of clearance flow on blade loading and losses. A three-dimensional Navier-Stokes code
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::005637d875b03490db9126daef233d23
https://doi.org/10.1115/91-gt-197
https://doi.org/10.1115/91-gt-197
Publikováno v:
29th Aerospace Sciences Meeting.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9ec83c8effa8a415f2861aa93c015c29
https://doi.org/10.2514/6.1991-341
https://doi.org/10.2514/6.1991-341