This thesis investigates the application of CFD techniques to the aerodynamic analysis of a U-shaped JETC. Investigations were carried out to determine the flow patterns present at a number of locations within the structure of a full U-shaped JETC. The CFD solutions produced in these investigations used recommendations from the literature in the set-up of the CFD solver, and provided the computational component towards problem-specific validation of the CFD techniques used. A structured series of CFD-aided investigation and design processes were then performed. These processes were based around a series of analyses that evaluated the influence of a number of cell parameters in terms of cell airflow efficiency and velocity distortion. Fo...
A method of providing ventilation using impinging jets (IJV) utilizes stratification while deliverin...
This project is concerned with CFD simulations of jets issued from elliptical nozzles. The investiga...
The design process of modern aircraft engines extensively makes use of computational fluid dynamics...
After overhaul or repair, turbofan engines are tested to ensure reliability and thrust meet safe sta...
This report investigates the characteristic fluid mechanical phenomena occurring on a diverterless c...
In the process of design, development and certification of a turbo-prop Light Transport Aircraft (LT...
The University of Leeds Formula Student Racing Team has recently included an aerodynamic package in ...
Scoops are important parts in an aircraft engine design, as they provide airflowto different equipme...
Thesis (M.S.)--Wichita State University, College of Engineering, Dept. of Aerospace EngineeringIn th...
In order to assist in the design of the aerodynamic shape of a closed circuit wind tunnel, which was...
This paper deals with the study of airflow in an uncluttered nacelle, as an important first step in ...
Aerodynamic integration of air intakes and the optimization of their performance are challenging tas...
In the last twenty years, CFD has evolved enormously and it is now used extensively by all turbomach...
With the increasing share of renewable power resources turbomachines need to be operated under a wid...
Intermediate turbine ducts are used in modern multi-spool jet engines for guiding the flow from the ...
A method of providing ventilation using impinging jets (IJV) utilizes stratification while deliverin...
This project is concerned with CFD simulations of jets issued from elliptical nozzles. The investiga...
The design process of modern aircraft engines extensively makes use of computational fluid dynamics...
After overhaul or repair, turbofan engines are tested to ensure reliability and thrust meet safe sta...
This report investigates the characteristic fluid mechanical phenomena occurring on a diverterless c...
In the process of design, development and certification of a turbo-prop Light Transport Aircraft (LT...
The University of Leeds Formula Student Racing Team has recently included an aerodynamic package in ...
Scoops are important parts in an aircraft engine design, as they provide airflowto different equipme...
Thesis (M.S.)--Wichita State University, College of Engineering, Dept. of Aerospace EngineeringIn th...
In order to assist in the design of the aerodynamic shape of a closed circuit wind tunnel, which was...
This paper deals with the study of airflow in an uncluttered nacelle, as an important first step in ...
Aerodynamic integration of air intakes and the optimization of their performance are challenging tas...
In the last twenty years, CFD has evolved enormously and it is now used extensively by all turbomach...
With the increasing share of renewable power resources turbomachines need to be operated under a wid...
Intermediate turbine ducts are used in modern multi-spool jet engines for guiding the flow from the ...
A method of providing ventilation using impinging jets (IJV) utilizes stratification while deliverin...
This project is concerned with CFD simulations of jets issued from elliptical nozzles. The investiga...
The design process of modern aircraft engines extensively makes use of computational fluid dynamics...