Author: Publisher:
ISBN:
Category : Mechanical engineering
Languages : en
Pages : 574
Book Description
ASME Technical Papers
Author: Publisher:
ISBN:
Category : Mechanical engineering
Languages : en
Pages : 574
Book Description
Journal of Turbomachinery
Author: Paper
Author: Publisher:
ISBN:
Category : Mechanical engineering
Languages : en
Pages : 576
Book Description
Pacific International Conference on Aerospace Science and Technology
Author: Heat Transfer in Gas Turbines
Author: Mingking K. ChyuPublisher:
ISBN:
Category : Science
Languages : en
Pages : 196
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
Heat Transfer in Gas Turbines
Author: Bengt SundénPublisher: Witpress
ISBN:
Category : Medical
Languages : en
Pages : 544
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.
Scientific and Technical Aerospace Reports
Author: Heat Transfer Measurements and Predictions on a Power Generation Gas Turbine Blade
Author: Publisher:
ISBN:
Category :
Languages : en
Pages : 22
Book Description
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.
International Aerospace Abstracts
Author: Advanced technologies in flow dynamics and combustion in propulsion and power, volume II
Author: Lei LuoPublisher: Frontiers Media SA
ISBN: 283251040X
Category : Technology & Engineering
Languages : en
Pages : 216
Book Description