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Author:
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ISBN:
Category : Mechanical engineering
Languages : en
Pages : 574
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Author:
Publisher:
ISBN:
Category : Mechanical engineering
Languages : en
Pages : 574
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Author:
Publisher:
ISBN:
Category : Turbomachines
Languages : en
Pages : 758
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Author:
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ISBN:
Category : Mechanical engineering
Languages : en
Pages : 576
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Author:
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ISBN:
Category : Astronautics
Languages : en
Pages : 500
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Author: Mingking K. Chyu
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 196
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Book Description
Comprises 15 papers presented at the November 1994 Congress. Contributors examine the complex nature of hot-side and cold-side heat transfer rates and distribution in papers representing three categories of gas turbine heat transfer: film-cooling, disk and gas-side heat transfer, and internal coolin
Author: Bengt Sundén
Publisher: Witpress
ISBN:
Category : Medical
Languages : en
Pages : 544
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Book Description
This title presents and reflects current active research on various heat transfer topics and related phenomena in gas turbine systems. It begins with a general introduction to gas turbine heat transfer, before moving on to specific areas.
Author:
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Category : Aeronautics
Languages : en
Pages : 836
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Author:
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ISBN:
Category :
Languages : en
Pages : 22
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Detailed heat transfer measurements and predictions are given for a power generation turbine rotor with 129 deg of nominal turning and an axial chord of 137 mm. Data were obtained for a set of four exit Reynolds numbers comprised of the design point of 628,000, -20%, +20%, and +40%. Three ideal exit pressure ratios were examined including the design point of 1.378, -10%, and +10%. Inlet incidence angles of 0 deg and +/-2 deg were also examined. Measurements were made in a linear cascade with highly three-dimensional blade passage flows that resulted from the high flow turning and thick inlet boundary layers. Inlet turbulence was generated with a blown square bar grid. The purpose of the work is the extension of three-dimensional predictive modeling capability for airfoil external heat transfer to engine specific conditions including blade shape, Reynolds numbers, and Mach numbers. Data were obtained by a steady-state technique using a thin-foil heater wrapped around a low thermal conductivity blade. Surface temperatures were measured using calibrated liquid crystals. The results show the effects of strong secondary vortical flows, laminar-to-turbulent transition, and also show good detail in the stagnation region.
Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 1020
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Author: Lei Luo
Publisher: Frontiers Media SA
ISBN: 283251040X
Category : Technology & Engineering
Languages : en
Pages : 216
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