Results 21 to 30 of about 135 (129)

[Retracted] Modeling and Optimization of Ship Waste Heat Utilization System Based on Genetic Algorithm and Sensing

open access: yesInternational Transactions on Electrical Energy Systems, Volume 2022, Issue 1, 2022., 2022
In order to solve the optimization problem of ship waste heat utilization system, the modeling and optimization method of ship waste heat utilization system based on genetic algorithm and sensing is proposed. The 6S50ME‐C8.2 volume method model was established based on Matlab/Simulink simulation platform.
Long Lyu, Nagamalai Vasimalai
wiley   +1 more source

Mild Detonation Initiation in Rotating Detonation Engines: An Experimental Study of the Deflagration-to-Detonation Transition in a Semiconfined Flat Slit Combustor with Separate Supplies of Fuel and Oxidizer

open access: yesAerospace, 2023
Rotating detonation engines (RDEs) are considered to be promising thrusters for aerospace propulsion. Detonation initiation in RDEs can be accompanied by a destructive explosion of an excess volume of the fuel mixture in the combustor.
Igor O. Shamshin   +5 more
doaj   +1 more source

Effect of Low Ambient Pressure on Spray Cone Angle of Pressure Swirl Atomizer

open access: yesInternational Journal of Aerospace Engineering, Volume 2021, Issue 1, 2021., 2021
Pressure swirl atomizers are widely used in gas turbine combustor; this paper is aimed at researching the effect of low ambient pressure (0.1 MPa to 0.01 MPa, lower than an atmosphere) on the spray cone angle of pressure swirl atomizer. The spray angle is captured by high‐speed photography; then, an image post program is used to process the spray angle
Zhengyan Guo   +8 more
wiley   +1 more source

Pressure Gain Characteristic of Continuously Rotating Detonation Combustion and its Influence on Gas Turbine Cycle Performance

open access: yesIEEE Access, 2018
Considering the pressure gain characteristic of continuously rotating detonation (CRD) combustion, a rotating detonation gas turbine cycle was established using methane as fuel.
Lei Qi   +4 more
doaj   +1 more source

Numerical Study on the Two-Phase Detonation Flow Field of Coal Powder-Hydrogen in a Rotating Detonation Engine [PDF]

open access: yesHangkong bingqi
Rotating detonation engines (RDEs) have attracted significant attention in the aerospace field due to their high thermal cycle efficiency. This study explores the characteristics of rotating detonation in gas-solid mixed fuel within an air atmosphere.
Weng Chunsheng, Ni Xiaodong, Xu Han
doaj   +1 more source

Effects of Annular Combustor Width on the Ethylene-Air Continuous Rotating Detonation

open access: yesInternational Journal of Aerospace Engineering, 2020
The realization and stable operation of Continuous Rotating Detonation (CRD) in the annular combustor fueled by hydrocarbon-air are still challenging.
Weijie Fan   +4 more
doaj   +1 more source

Effects of Inlet Condition Variations on the Operating Modes of Rotating Detonation Engines

open access: yes气体物理, 2023
In this study, the operating modes of the rotating detonation engine (RDE) under various inlet conditions were investigated numerically. It was shown that after the sudden reduction of the inlet total pressure, the resulting decrease of the mass flow ...
Song-bai YAO   +2 more
doaj   +1 more source

Effect of high-pressure detonation products on fuel injection and propagation characteristics of detonation wave

open access: yesPropulsion and Power Research, 2022
The effect of high-pressure detonation products on fuel injection and propagation characteristics of detonation wave has been investigated in the form of ion voltage by varying the equivalence ratio (ER), air mass flux, and operation duration with ...
Gaoyang Ge   +5 more
doaj   +1 more source

An alternative architecture of the Humphrey cycle and the effect of fuel type on its efficiency

open access: yesEnergy Science &Engineering, Volume 8, Issue 10, Page 3702-3716, October 2020., 2020
Novel Humphrey cycle architecture with stoichiometric combustor operation. Benchmarking of turbine plenum losses for pressure‐gain combustion cycles. Effect of internal irreversbilities of pressure‐gain combustion on cycle efficiency. Abstract Conventional gas turbines are a very mature technology, and performance improvements are becoming increasingly
Panagiotis Stathopoulos
wiley   +1 more source

Numerical Assessment of the Convective Heat Transfer in Rotating Detonation Combustors Using a Reduced-Order Model

open access: yesApplied Sciences, 2018
The pressure gain across a rotating detonation combustor offers an efficiency rise and potential architecture simplification of compact gas turbine engines.
James Braun   +2 more
doaj   +1 more source

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