Zobrazeno 1 - 10
of 33
pro vyhledávání: '"Laith Zori"'
Publikováno v:
Journal of Thermophysics and Heat Transfer. 37:404-423
This paper presents Ansys Fluent results for a rectangular exhaust nozzle test case from the Fifth AIAA Propulsion Aerodynamics Workshop. The main objective of the workshop was to assess the aerothermal interaction of a heated air exhaust with a film
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::711cb0533fa1515e31046d294e022f4c
https://doi.org/10.2514/1.t6595
https://doi.org/10.2514/1.t6595
Publikováno v:
Volume 6A: Heat Transfer — Combustors; Film Cooling.
One of the most effective ways to mitigate thermal fatigue in a high-pressure turbine’s blades is by cooling the blade from inside and outside via an intricate cooling system. The cooling flow passes from the blade interior through many small holes
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d1ef2af0c07085a7c1e3bbf283578738
https://doi.org/10.1115/gt2022-80700
https://doi.org/10.1115/gt2022-80700
Autor:
Thomas Biesinger, Maximilian Kölzer, Alexander Schukmann, Harald Roclawski, Marc Kainz, Philippe Godin, Juan Carlos Morales, Laith Zori
Publikováno v:
Volume 10D: Turbomachinery — Multidisciplinary Design Approaches, Optimization, and Uncertainty Quantification; Turbomachinery General Interest; Unsteady Flows in Turbomachinery.
This paper presents the application of the harmonic balance method to periodic turbomachinery flow problems containing multiple fundamental frequencies. It is well known that the solution convergence of a transient turbomachinery flow using classical
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3cc092292e085bc9bb90a14af128628f
https://doi.org/10.1115/gt2022-79393
https://doi.org/10.1115/gt2022-79393
Publikováno v:
Volume 10D: Turbomachinery — Multidisciplinary Design Approaches, Optimization, and Uncertainty Quantification; Turbomachinery General Interest; Unsteady Flows in Turbomachinery.
This paper continues previous research by the current authors in a series of papers describing the impact of multi-row interaction on the forced response behavior of embedded compressor rotors. Specifically, this work dives into an aspect of the embe
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9291eae94a899aa9510df54d319dedd4
https://doi.org/10.1115/gt2022-78101
https://doi.org/10.1115/gt2022-78101
Publikováno v:
Volume 10D: Turbomachinery — Multidisciplinary Design Approaches, Optimization, and Uncertainty Quantification; Turbomachinery General Interest; Unsteady Flows in Turbomachinery.
The current papers discuss the impact of separating the upstream and downstream forcing function contributions in an embedded compressor rotor. Previously, the authors have discussed separating the influence at a torsional mode crossing, and this pap
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f984f5c336409055f8f525a3197e7631
https://doi.org/10.1115/gt2022-78033
https://doi.org/10.1115/gt2022-78033
Publikováno v:
AIAA SCITECH 2022 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::649c49a44d9b7eb6208c407baad6e87f
https://doi.org/10.2514/6.2022-0221
https://doi.org/10.2514/6.2022-0221
Autor:
Valerio Viti, Krishna Zore, Laith Zori, Jean-Sebastien Cagnone, Anup Jain, Song Gao, John Stokes
Publikováno v:
AIAA AVIATION 2021 FORUM.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1336903b8fc6f45a9d171b1e5c67b76b
https://doi.org/10.2514/6.2021-2506
https://doi.org/10.2514/6.2021-2506
Publikováno v:
Volume 2D: Turbomachinery — Multidisciplinary Design Approaches, Optimization, and Uncertainty Quantification; Radial Turbomachinery Aerodynamics; Unsteady Flows in Turbomachinery.
Modeling the interaction between gas turbine engine modules is complex. The compact nature of modern engines makes it difficult to identify an optimal interface location between components, especially in the hot section. The combustor and high-pressu
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d4873e553516a744d6652437baff32e9
https://doi.org/10.1115/gt2021-59344
https://doi.org/10.1115/gt2021-59344
Publikováno v:
Volume 9A: Structures and Dynamics — Aerodynamics Excitation and Damping; Bearing and Seal Dynamics; Emerging Methods in Design and Engineering.
This paper focuses on the impact of hub labyrinth seal leakage flows on the aeromechanical behavior of an embedded compressor rotor. End wall flows are critical in determining the performance of gas turbine engine compressors, particularly the hub le
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::81b7df2134bf86bdc20dd0a95921f977
https://doi.org/10.1115/gt2021-58779
https://doi.org/10.1115/gt2021-58779
Publikováno v:
AIAA Scitech 2021 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::21582b26eac0c50cb950ad0dabbb60e3
https://doi.org/10.2514/6.2021-1073
https://doi.org/10.2514/6.2021-1073