Zobrazeno 1 - 10
of 13
pro vyhledávání: '"David E. Halstead"'
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:
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
Publikováno v:
37th Aerospace Sciences Meeting and Exhibit.
Experimental data from jet-engine tests have indicated that unsteady blade row interactions and separation can have a significant impact on the efficiency of low-pressure turbine stages. Measured turbine efficiencies at takeoff can be as much as two
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d65f1fd49566e3f3acc99aba1b47c8f7
https://doi.org/10.2514/6.1999-742
https://doi.org/10.2514/6.1999-742
Autor:
Hyoun-Woo Shin, David E. Halstead, Howard P. Hodson, Gregory J. Walker, Theodore H. Okiishi, D. C. Wisler
Publikováno v:
Volume 1: Turbomachinery.
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_________::4d6ecaacfeb7020fa19d3e1ba3477ec3
https://doi.org/10.1115/95-gt-462
https://doi.org/10.1115/95-gt-462
Autor:
Hyoun-Woo Shin, Howard P. Hodson, Gregory J. Walker, Theodore H. Okiishi, D. C. Wisler, David E. Halstead
Publikováno v:
Volume 1: Turbomachinery.
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_________::5d5b4a005807ff7696a2aa37ac9e6352
https://doi.org/10.1115/95-gt-461
https://doi.org/10.1115/95-gt-461
Autor:
Hyoun-Woo Shin, Gregory J. Walker, David E. Halstead, D. C. Wisler, Howard P. Hodson, Theodore H. Okiishi
Publikováno v:
Volume 1: Turbomachinery.
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_________::a0690d14101f565f049ad2f3b70d49e5
https://doi.org/10.1115/95-gt-464
https://doi.org/10.1115/95-gt-464
Autor:
Hyoun-Woo Shin, Theodore H. Okiishi, Gregory J. Walker, David E. Halstead, D. C. Wisler, Howard P. Hodson
Publikováno v:
Volume 1: Turbomachinery.
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_________::5531028b56d9269c7deeaec680fd39b3
https://doi.org/10.1115/95-gt-463
https://doi.org/10.1115/95-gt-463