Results 161 to 170 of about 34,180 (208)
Solubility and Diffusion of Main Biogas Components in a Glassy Polysulfone-Based Membrane. [PDF]
Tańczyk M +5 more
europepmc +1 more source
Sustainable Infrastructure: Recycled Concrete Aggregates for Cycle Paths. [PDF]
Konca P +7 more
europepmc +1 more source
A review on aero-engine inlet-compressor integration and inlet flow distortion in axial compressors. [PDF]
Li Z, Sun D, Dong X, Sun X.
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Unsteady CFD of a marine current turbine using OpenFOAM with generalised grid interface
Humphrey, V.F. +2 more
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2021
The book is divided into eight chapters. Chapter 1 is an introductory chapter and is a synthesis of the book titled Lecture notes on Fluid Machines—M. Gambini, M. Vellini (in Italian), 2007, adopted for the Turbomachinery and Energy Systems courses for students of the bachelor’s Degree in Mechanical and Energy Engineering of the University of Rome Tor ...
Gambini, Marco, Vellini, Michela
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The book is divided into eight chapters. Chapter 1 is an introductory chapter and is a synthesis of the book titled Lecture notes on Fluid Machines—M. Gambini, M. Vellini (in Italian), 2007, adopted for the Turbomachinery and Energy Systems courses for students of the bachelor’s Degree in Mechanical and Energy Engineering of the University of Rome Tor ...
Gambini, Marco, Vellini, Michela
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2023
Implementation of a Combustion Module within the Nektar++ FrameworkCombustion modelling methods are implemented into the Nektar++ framework to create a reactive flow solver capable of accurately modelling combustion flow regimes at low Mach numbers. The study investigates how the high-order resolution of a mixing flow field translates to modelling of ...
Aidan Forknall +2 more
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Implementation of a Combustion Module within the Nektar++ FrameworkCombustion modelling methods are implemented into the Nektar++ framework to create a reactive flow solver capable of accurately modelling combustion flow regimes at low Mach numbers. The study investigates how the high-order resolution of a mixing flow field translates to modelling of ...
Aidan Forknall +2 more
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Aeronautical Quarterly, 1977
SummaryTwo methods of analysis are developed for the unsteady wave flow through axial turbomachinery of high hub-tip ratio. In the first method, the machine is supposed to consist of an infinite number of small stages. Differential equations for the instantaneous values of flow properties are derived which may be solved directly or by the method of ...
J H Horlock, H Daneshyar
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SummaryTwo methods of analysis are developed for the unsteady wave flow through axial turbomachinery of high hub-tip ratio. In the first method, the machine is supposed to consist of an infinite number of small stages. Differential equations for the instantaneous values of flow properties are derived which may be solved directly or by the method of ...
J H Horlock, H Daneshyar
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Tribology, 1968
The paper presents gas bearing turbomachinery developments for the past decade. With the aid of examples of eight different requirements, it answers the question: “Why Gas-Bearing Turbomachinery?” These examples cover: No Contamination, high efficiency, low temperature, high temperature, radiation damage, reliability and long life, high speed and long ...
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The paper presents gas bearing turbomachinery developments for the past decade. With the aid of examples of eight different requirements, it answers the question: “Why Gas-Bearing Turbomachinery?” These examples cover: No Contamination, high efficiency, low temperature, high temperature, radiation damage, reliability and long life, high speed and long ...
openaire +1 more source
Accelerating Turbomachinery Design
Volume 5: Turbo Expo 2002, Parts A and B, 2002It is widely accepted that a company’s market penetration, and hence its profitability, is very closely linked to the speed with which it can produce a new design. This paper describes a method which aims to assist the designer in producing higher performance turbomachinery designs more quickly by accelerating the process by which they are produced ...
Jerome P. Jarrett +2 more
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