Zobrazeno 1 - 10
of 42
pro vyhledávání: '"D. C. Wisler"'
Autor:
Z. S. Spakovszky, Hyoun-Woo Shin, Seung Jin Song, B. F. Beacher, Albert Frank Storace, F. F. Ehrich, Manuel Martinez-Sanchez, D. C. Wisler
Publikováno v:
Journal of Turbomachinery. 123:433-445
An experimental and theoretical investigation has been conducted to evaluate the effects seen in axial-flow compressors when the centerline of the rotor is displaced from the centerline of the static structure of the engine. This creates circumferent
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9140a0afd2eee3e4e9d7e42c8ec59e62
https://doi.org/10.1115/1.1378299
https://doi.org/10.1115/1.1378299
Autor:
Seung Jin Song, Hyoun-Woo Shin, Albert Frank Storace, D. C. Wisler, F. F. Ehrich, Z. S. Spakovszky, B. F. Beacher, Manuel Martinez-Sanchez
Publikováno v:
Journal of Turbomachinery. 123:446-452
An experimental and theoretical investigation was conducted to evaluate the effects seen in axial-flow compressors when the centerline of the rotor becomes displaced from the centerline of the static structure of the engine, thus creating circumferen
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::979e9c1c73c98840393cd22f60ea64ef
https://doi.org/10.1115/1.1370165
https://doi.org/10.1115/1.1370165
Publikováno v:
Journal of Propulsion and Power. 16:160-163
Experimental data from jet-engine tests have indicated that unsteady blade row (wake) interactions and separation can have a significant impact on the efficiency of turbine stages. The effects of these interactions can be intensified in low-pressure
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::04a8ee18334807bfaf858977b092617f
https://doi.org/10.2514/2.5550
https://doi.org/10.2514/2.5550
Autor:
Hyoun-Woo Shin, Frank E. Marble, Edward M. Greitzer, D. C. Wisler, M. B. Graf, T. S. Wong, Choon S. Tan
Publikováno v:
Journal of Turbomachinery. 120:648-661
The effects of circumferentially nonuniform tip clearance on axial compressor performance and stability have been investigated experimentally and analytically. A theoretical model for compressor behavior with nonaxisymmetric tip clearance has been de
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::17ea1c381f7b4c312dfb0b45ff1587c7
https://doi.org/10.1115/1.2841774
https://doi.org/10.1115/1.2841774
Autor:
Theodore H. Okiishi, Howard P. Hodson, Hyoun-Woo Shin, David E. Halstead, Gregory J. Walker, D. C. Wisler
Publikováno v:
Journal of Turbomachinery. 119:426-444
This is Part Two of a four-part paper. It begins with Section 6.0 and continues to describe the comprehensive experiments and computational analyses that have led to a detailed picture of boundary layer development on airfoil surfaces in multistage t
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ff132a9f86d7905ce81c15f185f7738c
https://doi.org/10.1115/1.2841142
https://doi.org/10.1115/1.2841142
Autor:
Hyoun-Woo Shin, Gregory J. Walker, D. C. Wisler, Howard P. Hodson, Theodore H. Okiishi, David E. Halstead
Publikováno v:
Journal of Turbomachinery. 119:225-237
This is Part Three of a four-part paper. It begins with Section 11.0 and continues to describe the comprehensive experiments and computational analyses that have led to a detailed picture of boundary layer development on airfoil surfaces in multistag
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::dcdcc5e4156586f7e413fbb89bc2e23e
https://doi.org/10.1115/1.2841105
https://doi.org/10.1115/1.2841105
Autor:
Hyoun-Woo Shin, Gregory J. Walker, D. C. Wisler, Howard P. Hodson, David E. Halstead, Theodore H. Okiishi
Publikováno v:
Journal of Turbomachinery. 119:128-139
This is Part Four of a four-part paper. It begins with Section 16.0 and concludes the description of the comprehensive experiments and computational analyses that have led to a detailed picture of boundary layer development on airfoil surfaces in mul
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::86391cf8fd3dac3b94a9e5daa83ab058
https://doi.org/10.1115/1.2841001
https://doi.org/10.1115/1.2841001
Autor:
Hyoun-Woo Shin, Theodore H. Okiishi, Gregory J. Walker, D. C. Wisler, Howard P. Hodson, David E. Halstead
Publikováno v:
Journal of Turbomachinery. 119:114-127
Comprehensive experiments and computational analyses were conducted to understand boundary layer development on airfoil surfaces in multistage, axial-flow compressors and LP turbines. The tests were run over a broad range of Reynolds numbers and load
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a0ff4828a72b5201af08d85397da6a8e
https://doi.org/10.1115/1.2841000
https://doi.org/10.1115/1.2841000
Autor:
Hyoun-Woo Shin, I. J. Day, P. D. Silkowski, Edward M. Greitzer, C. S. Tan, J. P. Longley, D. C. Wisler, R. E. Plumley
Publikováno v:
Journal of Turbomachinery. 118:181-188
In multispool engines, rotating stall in an upstream compressor will impose a rotating distortion on the downstream compressor, thereby affecting its stability margin. In this paper experiments are described in which this effect was simulated by a ro
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::dfe4f94676655c796900138bf9763046
https://doi.org/10.1115/1.2836624
https://doi.org/10.1115/1.2836624
Autor:
D. C. Wisler
Publikováno v:
Journal of Turbomachinery. 134
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::946b0c46e0c5097e42fcfa0a07fd33b8
https://doi.org/10.1115/1.4007211
https://doi.org/10.1115/1.4007211