Zobrazeno 1 - 10
of 27
pro vyhledávání: '"W. C. Zierke"'
Autor:
W. A. Straka, W. C. Zierke
Publikováno v:
Journal of Propulsion and Power. 12:250-259
Surface flow visualization on an axial-flow pump results in patterns of the skin-friction lines on various surfaces and these patterns provide important insight into the topology of the three-dimensional flowfield. In particular, critical points and
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7b13982e5cc1091c67f5e3f267bf2939
https://doi.org/10.2514/3.24021
https://doi.org/10.2514/3.24021
Publikováno v:
Journal of Turbomachinery. 117:522-532
A high-Reynolds-number pump (HIREP) facility has been used to acquire flow measurements in the rotor blade tip clearance region, with blade chord Reynolds numbers of 3,900,000 and 5,500,000. The initial experiment involved rotor blades with varying t
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::977e0873fbaabc752ff09937e6241e26
https://doi.org/10.1115/1.2836564
https://doi.org/10.1115/1.2836564
Publikováno v:
Journal of Fluids Engineering. 117:485-490
The high Reynolds number pump (HIREP) facility at ARL Penn State has been used to perform a low-speed, large-scale experiment of the incompressible flow of water through a two-blade-row turbomachine. The objectives of this experiment were to provide
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a6302a807cdacee376cc02b3a24545d6
https://doi.org/10.1115/1.2817288
https://doi.org/10.1115/1.2817288
Autor:
Steven Deutsch, W. C. Zierke
Publikováno v:
Journal of Turbomachinery. 112:241-255
Measurements, made with laser Doppler velocimetry, about a double-circular-arc compressor blade in cascade are presented for −1.5 and −8.5 deg incidence angles and a chord Reynolds number near 500,000. Comparisons between the results of the curre
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0e45689c407ad78b56da882a7bdcfaab
https://doi.org/10.1115/1.2927638
https://doi.org/10.1115/1.2927638
Publikováno v:
Volume 1: Turbomachinery.
A high Reynolds number pump (HIREP) facility has been used to acquire flow measurements in the rotor blade tip clearance region-with blade chord Reynolds numbers of 3,900,000 and 5,500,000. The initial experiment involved rotor blades with varying ti
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7e86dd5c8627459cb4fbe885a5306a18
https://doi.org/10.1115/94-gt-453
https://doi.org/10.1115/94-gt-453
Publikováno v:
Volume 1: Turbomachinery.
A high Reynolds number pump (HIREP) facility has been used to acquire flow measurements in the rotor blade tip clearance region-with blade chord Reynolds numbers of 3,900,000 and 5,500,000. The initial experiment involved rotor blades with varying ti
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e16881f8b2d3d6502ddd8720a035a3a4
https://doi.org/10.1115/94-gt-454
https://doi.org/10.1115/94-gt-454
Autor:
W. C. Zierke, Steven Deutsch
Publikováno v:
Journal of Turbomachinery. 113:571-572
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2b73f61300f92dddeb83239395905ee9
https://doi.org/10.1115/1.2929116
https://doi.org/10.1115/1.2929116
Autor:
W. C. Zierke
Publikováno v:
Journal of Turbomachinery. 118:248-248
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4a2367003990a344280f5c08ff52fcb6
https://doi.org/10.1115/1.2836632
https://doi.org/10.1115/1.2836632
Autor:
W. C. Zierke, Steven Deutsch
Publikováno v:
Journal of Turbomachinery. 110:138-145
Using the facility described in Part 1 [29], eleven detailed velocity and turbulence intensity profiles are obtained on the suction surface of a double circular arc blade in cascade. At the measured incidence angle of 5 deg, transition through a lead
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::136c28664c7c92c68c3f3a86c040595f
https://doi.org/10.1115/1.3262159
https://doi.org/10.1115/1.3262159
Autor:
W. C. Zierke, Steven Deutsch
Publikováno v:
Journal of Turbomachinery. 110:146-152
Using the facility described in Part 1 [23], 11 detailed velocity and turbulence intensity profiles are obtained on the pressure surface of a double circular arc compressor blade in cascade. Two profiles are obtained in the near wake. Laminar boundar
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::50838c0595eab7a94a433c5cfa5b5936
https://doi.org/10.1115/1.3262160
https://doi.org/10.1115/1.3262160