Results 11 to 20 of about 93,646 (365)

Study on Unstable Combustion Characteristics of Model Combustor with Different Swirler Schemes

open access: yesEnergies, 2022
In this paper, the effect of the swirler scheme on combustion instability is studied. Through the proper orthogonal decomposition (POD) of flame images, Abel inverse transform and other methods, the influence of swirl intensity on the characteristic ...
Jiangang Hao   +6 more
doaj   +1 more source

Effect of associated gas utilization on the creep life of gas turbines employed for power generation application

open access: yesResults in Engineering, 2023
Utilizing associated gas (A-Gas) in gas turbines for power generation applications would greatly solve some of the acute power challenges Nigeria is faced with over the years.
Roupa Agbadede   +2 more
doaj   +1 more source

The Outlook of TBCC Integrated Energy Based on theSecondary Power System

open access: yesHangkong gongcheng jinzhan, 2019
The electrical generation, hydraulic power and pneumatic power of an aircraft is supplied by the secondary power system or the power extracted from engines by the secondary power system.
Wang Wei, Dong Aiqun, Li Dan
doaj   +1 more source

Shear Layer Instability of Flow Around a Circular Cylinder Based on Large Eddy Simulation

open access: yesShanghai Jiaotong Daxue xuebao, 2021
The flow around a cylinder is a common research object of fluid mechanics. As the Reynolds number (Re) increases, the Kelvin-Helmholtz instability of the shear layer will occur in the wake behind the cylinder.
GUO Zhiyuan, YU Peixiang, OUYANG Hua
doaj   +1 more source

The WISC Gas Turbine Engine [PDF]

open access: yesVolume 2: Coal, Biomass and Alternative Fuels; Combustion and Fuels; Oil and Gas Applications; Cycle Innovations, 1997
Combined gas turbine-steam turbine cycles have gained widespread acceptance as the most efficient utilization of the gas turbine for power generation, particularly for large power plants. In order to maximize the achievable thermal efficiency, more than one exhaust heat recovery boiler is used.
A. Radey Shouman, A. R. Shouman
openaire   +1 more source

Recursive least squares for online dynamic identification on gas turbine engines [PDF]

open access: yes, 2016
Online identification for a gas turbine engine is vital for health monitoring and control decisions because the engine electronic control system uses the identified model to analyze the performance for optimization of fuel consumption, a response to ...
Nalianda, Devaiah   +2 more
core   +1 more source

Simulation study on exhaust turbine power generation for waste heat recovery from exhaust of a diesel engine

open access: yesEnergy Reports, 2021
Diesel engine has been used as the primary mover in vehicles for a long time. It is known that around 25%–30% of the fuel energy is wasted in the exhaust gas from diesel engines.
Yongming Xu   +3 more
doaj   +1 more source

Choice of gas temperature at the turbopump turbine inlet

open access: yesВестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, 2022
The article considers some issues of choosing the gas temperature at the inlet of a liquid rocket engine turbopump turbine. The turbine is one of the key elements of the engine and its operability depends on the gas temperature.
A. V. Ivanov
doaj   +1 more source

Exergetic, exergoeconomic and exergoenvironmental analysis of intercooled gas turbine engine [PDF]

open access: yes, 2016
Exergetic and exergoeconomic and exergoenvironmental analyses have been performed for an advanced aero-derivative intercooled gas turbine engine. The proposed system was modelled using the IPSEpro software package and validated using manufacturer’s ...
Al-Mutawa, Nawaf   +2 more
core   +1 more source

CONTROLLER DESIGN FOR A GAS TURBINE ENGINE

open access: yesIFAC Proceedings Volumes, 1979
Abstract An aircraft gas turbine engine is modelled as a multivariable system of nonlinear dynamic equations which is subject to a number of operating restrictions. This paper considers the specific control problem of transferring the states of the engine from an operating point of low thrust to high thrust output in an optimal manner (transient mode)
C.W. Jones, P.J. Fleming
openaire   +1 more source

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