Zobrazeno 1 - 10
of 11
pro vyhledávání: '"K. C. Civinskas"'
Publikováno v:
Journal of Propulsion and Power. 11:213-220
When computing flows inside geometrically complex turbine-blade coolant passages, the structure of the grid system used can significantly affect the overall time and cost required to obtain solutions. This article addresses this issue while evaluatin
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d747d28a07f756f8ced4a213c49bc60e
https://doi.org/10.2514/3.51413
https://doi.org/10.2514/3.51413
Publikováno v:
Journal of Propulsion and Power. 6:598-611
The operating conditions and the propellant transport properties used in Earth-to-orbit (ETO) applications affect the aerothermodynamic design of ETO turbomachinery in a number of ways. This paper discusses some aerodynamic and heat-transfer implicat
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b158cf6bff0df6e596cc614a10579755
https://doi.org/10.2514/3.23261
https://doi.org/10.2514/3.23261
Publikováno v:
Volume 3: Heat Transfer; Electric Power; Industrial and Cogeneration.
Detailed heat transfer measurementa and predictions are given for a turbine rotor with 136° of turning and an axial chord of 12.7 cm. Data were obtained for inlet Reynolds numbers of 0.5 and 1.0 × 106, for isentropic exit Mach numbers of 1.0 and 1.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::30681a7625d3fdb2fe566d0ece31bdb1
https://doi.org/10.1115/99-gt-125
https://doi.org/10.1115/99-gt-125
Publikováno v:
Volume 4: Heat Transfer; Electric Power; Industrial and Cogeneration.
Computations were performed to study the three-dimensional flow and heat transfer in a ribbed U-shaped duct of square cross section under operating conditions that are typical of industrial gas turbines. Basically, all walls were maintained at a temp
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6b27bb59ac530e69eee50cafb48edbb2
https://doi.org/10.1115/98-gt-213
https://doi.org/10.1115/98-gt-213
Publikováno v:
32nd Joint Propulsion Conference and Exhibit.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ee0a2b4f00f7c4dd4a5019815f5261a2
https://doi.org/10.2514/6.1996-3163
https://doi.org/10.2514/6.1996-3163
Publikováno v:
32nd Joint Propulsion Conference and Exhibit.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7eca1d1c215576a8b72f21ac69a58caf
https://doi.org/10.2514/6.1996-3161
https://doi.org/10.2514/6.1996-3161
Publikováno v:
29th Joint Propulsion Conference and Exhibit.
When computing flows inside geometrically complex turbine-blade coolant passages, the structure of the grid system used can affect significantly the overall time and cost required to obtain solutions. This paper addresses this issue while evaluating
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d9ac12508b73d96020b43836fd78a937
https://doi.org/10.2514/6.1993-2559
https://doi.org/10.2514/6.1993-2559
Publikováno v:
Volume 4: Heat Transfer; Electric Power; Industrial and Cogeneration.
Time-averaged Stanton number and surface-pressure distributions are reported for the first-stage vane row and the first-stage blade row of the Rocketdyne Space Shuttle Main Engine two-stage fuel-side turbine. These measurements were made at 10, 50, a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::b6b67f9c3d09068d6ab1c4c17226be3e
https://doi.org/10.1115/92-gt-194
https://doi.org/10.1115/92-gt-194
Publikováno v:
Journal of Propulsion and Power. 4:541-548
Comparisons are made between calculated and measured heat-transfer distributions on the midspan locations of the stators and rotors of two turbine stages. The agreement is generally good, except in regions near the leading edge, and is better for bla
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::453fb0e1d8d71f78761b97fbeb3ad170
https://doi.org/10.2514/3.23098
https://doi.org/10.2514/3.23098
Publikováno v:
24th Joint Propulsion Conference.
The operating conditions and the propellant transport properties used in Earth-to-Orbit (ETO) applications affect the aerothermodynamic design of ETO turbomachinery in a number of ways. Some aerodynamic and heat transfer implications of the low molec
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ce28121ef0404ab600e59db727a5fcb6
https://doi.org/10.2514/6.1988-3091
https://doi.org/10.2514/6.1988-3091