Zobrazeno 1 - 9
of 9
pro vyhledávání: '"Michael Macrorie"'
Autor:
Nicholas H. Maher, Mark H. Ross, Scott C. Morris, Stephan Priebe, Giridhar Jothiprasad, David Allan, Gregory McNulty, Michael Macrorie, Ramakrishna Mallina
Publikováno v:
Journal of Turbomachinery. 145
An advanced casing treatment (CT) design was tested in a single-stage, high-speed axial compressor. The geometry of the casing included bent-axial slots applied near the rotor leading edge. Compressor performance and stall margin (SM) measurements we
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7909b477c3009ce47644b8dc3ed583f3
https://doi.org/10.1115/1.4056699
https://doi.org/10.1115/1.4056699
Autor:
Nicholas H. Maher, Mark H. Ross, Scott C. Morris, Stephan Priebe, Giridhar Jothiprasad, David Allan, G. Scott McNulty, Michael Macrorie
Publikováno v:
Volume 10A: Turbomachinery — Axial Flow Fan and Compressor Aerodynamics.
An advanced casing treatment design, in the form of bent-axial slots applied to the casing near the rotor leading edge, was tested in a single stage high speed axial compressor. Compressor performance and stall margin measurements were acquired for b
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::00bb2eec849852a80ce2416eb894c948
https://doi.org/10.1115/gt2022-83459
https://doi.org/10.1115/gt2022-83459
Characterization and Impact of Secondary Flows in a Discrete Passage Centrifugal Compressor Diffuser
Publikováno v:
Volume 2B: Turbomachinery.
Truncating the exit of a discrete passage centrifugal compressor diffuser is observed to enhance a research compressor’s stall line. By interrogating the experimental data along with a set of well-designed Reynolds-Averaged Navier Stokes computatio
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::e88b1618e1c19a3e33a84461d938c63d
https://doi.org/10.1115/gt2018-76231
https://doi.org/10.1115/gt2018-76231
Autor:
Wayne R. Pauley, Michael Macrorie
Publikováno v:
AIAA Journal. 33:1383-1390
The interaction between propagating spanwise vortices and a turbulent boundary layer was studied experimentally. The results focus on the relationship between the passage of vortex structures and the response of the boundary layer in terms of ensembl
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::27159bd73b8980753a884788223930dc
https://doi.org/10.2514/3.12686
https://doi.org/10.2514/3.12686
Publikováno v:
Volume 6: Turbo Expo 2007, Parts A and B.
Unsteady numerical simulations in a centrifugal compressor stage consisting of an impeller followed by a discrete passage diffuser are employed to characterize unsteady impeller blade loading. For a stage typical of modern design, peak dynamic loads
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6e1ab38264fc5cc6fe6d25c611a519d2
https://doi.org/10.1115/gt2007-28002
https://doi.org/10.1115/gt2007-28002
Publikováno v:
22nd Applied Aerodynamics Conference and Exhibit.
Impeller and diffuser interaction effects in a centrifugal compressor stage, steady or unsteady, has been a subject of considerable interest to a designer to quantify the extent of technology advancement that can be achieved. Component optimization C
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::31484e855388d59d07eb66ef8e344e27
https://doi.org/10.2514/6.2004-4835
https://doi.org/10.2514/6.2004-4835
Autor:
Michael Macrorie, Wayne R. Pauley
Publikováno v:
31st Aerospace Sciences Meeting.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::79b875dcdf33fdd6eba54c7c90fb3210
https://doi.org/10.2514/6.1993-552
https://doi.org/10.2514/6.1993-552
Autor:
Michael Macrorie, Wayne R. Pauley
Publikováno v:
10th Applied Aerodynamics Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3b444f897db46b0ccdd1df10a8871860
https://doi.org/10.2514/6.1992-2688
https://doi.org/10.2514/6.1992-2688
Publikováno v:
The Journal of the Acoustical Society of America. 89:1944-1944
A new technique is being investigated for the direct measurement of surface stresses (both pressure and shear) in Steady and unsteady wall bounded flows. The technique utilizes surface acoustic wave (SAW) devices. A first generation sensor has been u
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::94733ea3d509fc4523508d13e623b348
https://doi.org/10.1121/1.2029618
https://doi.org/10.1121/1.2029618