Results 1 to 10 of about 512 (187)
International Journal of Aerospace Engineering, 2022 In order to rapidly predict the performance of hydrocarbon-fueled regeneratively cooled scramjet engine in system design, a quasi-one-dimensional model has been developed.
Yuefei Xiong +4 more
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Applications in Energy and Combustion Science, 2021 The development of liquid ammonia spray combustion technology is expected to reduce the cost and size of gas turbines otherwise fueled with gaseous ammonia. However, successful studies on this topic are scarce due to the difficulty in flame stabilization.
Ekenechukwu C. Okafor +9 more
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Experimental study of the effect of swirling inflow on film cooling effectiveness
Case Studies in Thermal Engineering, 2022 Lean burn combustor can save fuel and reduce pollutant emissions. The exit of the lean burn combustor generates strong swirling flow, which has a significant influence on the heat transfer performance of the downstream turbine.
Zhuang Wu +4 more
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Evaluation of Cooling Requirements for Rotating Detonation Combustors
Volume 7A: Heat Transfer — Combustors; Film Cooling, 2023 Abstract In the last decade, the Rotating Detonation Combustor (RDC) has received growing attention among the different Pressure Gain Combustion concepts due to the simplicity of the design and the potential ease of integration in gas turbines.
Sandri U. +5 more
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Improved Wall Temperature Prediction for the LUMEN Rocket Combustion Chamber with Neural Networks
Aerospace, 2023 Accurate calculations of the heat transfer and the resulting maximum wall temperature are essential for the optimal design of reliable and efficient regenerative cooling systems.
Kai Dresia +3 more
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Energy Reports, 2022 This paper adopts the exergy analysis method of second law of thermodynamics to analyze the characteristics of off-design conditions of distributed combined cooling, heat and power system (CCHP).
Youyuan Shao +4 more
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Experimental Investigation of a Fuel Cooled Combustor: Cooling Efficiency and Coke Formation [PDF]
21st AIAA International Space Planes and Hypersonics Technologies Conference, 2017 Scramjet is an air-breathing engine designed to propel advanced aircrafts in the atmosphere, suitable, according to various studies, to thrust high-speed hypersonic flights (over Mach 5). The thermal protection of vehicles flying at hypersonic velocities is a critical problem; as at supersonic speeds the incoming air is at too high temperature to be ...
Taddeo, L. +6 more
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Investigation of the acoustics of full-scale perforated liners in gas turbine combustors
Fuel Communications, 2022 In conventional gas turbine combustors, the combustion chamber linings are perforated and used for cooling. To cool the liner evenly, bias flows are introduced into the combustor at rates that depend on the operating condition.
Abdullah Shahjalal, Lam Hak-Keung
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Case Studies in Thermal Engineering, 2014 This study was performed to investigate the effects of cylindrical and row trenched cooling holes with alignment angles of 0° and 90° at blowing ratio of 3.18 on the film cooling performance adjacent to the endwall surface of a combustor simulator.
Ehsan Kianpour, Nor Azwadi Che Sidik
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Heat Pipe Combustor Cooling [PDF]
Volume 4: Heat Transfer; Electric Power; Industrial and Cogeneration, 1998 The general approach which has been taken toward cooling aircraft turbine combustor liners is to utilize a portion of incoming combustor air for film-cooling. In this paper an alternate cooling method is considered, which is referred to as Heat Pipe Combustor Cooling.
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