Zobrazeno 1 - 10
of 418
pro vyhledávání: '"E. M. Greitzer"'
Autor:
Yiannis Andreopoulos
Publikováno v:
Journal of Fluid Mechanics. 533
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::38968f8909a39aec44a528786881f3f9
https://doi.org/10.1017/s0022112005214982
https://doi.org/10.1017/s0022112005214982
Publikováno v:
Journal of Turbomachinery. 145
This paper presents an assessment of the effect of nonaxisymmetric fan exit guide vanes (FEGVs) to mitigate, or even reduce to zero, the impact of circumferential flow distortion—such as created by boundary layer ingestion (BLI)—on fan rotor effi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a2757b5a4d32cb1fa1f58b143c722404
https://doi.org/10.1115/1.4055645
https://doi.org/10.1115/1.4055645
Publikováno v:
Journal of Turbomachinery. 144
This article presents first-of-a-kind measurements, and complementary computations, of the flow through the propulsion system of a boundary layer ingesting, twin-engine advanced civil transport aircraft configuration. The experiments were carried out
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::528ce0f22fb02a77859493c9752cfd14
https://doi.org/10.1115/1.4054035
https://doi.org/10.1115/1.4054035
Autor:
D. E. Newland, E. M. Greitzer
Publikováno v:
Biographical Memoirs of Fellows of the Royal Society. 66:309-328
William Rede Hawthorne was a pioneer in gas turbine aerodynamics and thermodynamics, a sought-after technology advisor to industry and government, and a generous and enthusiastic teacher who encouraged students to excel. His outstanding contributions
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5db5bdb0925108ca6bb09b21e4410e79
https://doi.org/10.1098/rsbm.2017.0036
https://doi.org/10.1098/rsbm.2017.0036
A Computational Model for Short-Wavelength Stall Inception and Development in Multistage Compressors
Publikováno v:
Journal of Turbomachinery. 121:726-734
This paper presents a computational model for simulating axial compressor stall inception and development via disturbances with length scales on the order of several (typically about three) blade pitches. The model was designed for multistage compres
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::222e67240a86c8e717c2c51744f1604a
https://doi.org/10.1115/1.2836726
https://doi.org/10.1115/1.2836726
Publikováno v:
Journal of Turbomachinery. 120:431-439
This paper describes the first experimental validation of transfer function modeling and active stabilization for axial compressors with circumferential inlet distortion. The inlet distortion experiments were carried out in a three-stage low-speed co
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c9b1a301af3640ed2632ebf44f45d31c
https://doi.org/10.1115/1.2841734
https://doi.org/10.1115/1.2841734
Publikováno v:
Volume 8: Turbomachinery, Parts A, B, and C.
In this paper we describe the structures that produce a spike-type 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
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::41c3fafde31761ae8681b5761a0d05e3
https://doi.org/10.1115/gt2012-68707
https://doi.org/10.1115/gt2012-68707
Publikováno v:
Volume 7: Turbomachinery, Parts A and B.
This paper provides a physical interpretation of the mechanism of stagnation enthalpy and stagnation pressure changes in turbomachines due to unsteady flow, the agency for all work transfer between a turbomachine and an inviscid fluid. Examples are f
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::395e95e780b4c9c09aaca4771b9af0ae
https://doi.org/10.1115/gt2009-59374
https://doi.org/10.1115/gt2009-59374
