An investigation of the flow fields of mesoscale inlet guide vanes is presented in this paper. An in depth look at the design process is also presented. The guidelines set in place for the design and manufacturing of standard equipment were utilized with discretion. The parameters that were to be achieved for these designs were to keep the inlet vanes within a 1 to 2cm tip diameter range. The difficulty with this is the manufacturability of something so small. In order to ease this problem the vanes were scaled to be twice as large as the original design size while keeping the hub the same diameter. This allowed the vanes to remain intact during the manufacturing process. After the design was completed and the parts had been manufactured a ...
As ke Thorlund for valuable comments on the design of guide vanes. We are grateful to Mr. Ulf Landé...
Various experimental and numerical studies of advanced blade configurations for variable inlet guide...
The article describes the research on the intake manifold for ultralight aircraft engine Vaxell 100i...
An investigation of the flow fields of mesoscale inlet guide vanes is presented in this paper. An in...
In Francis turbine, a small clearance gap between the guide vanes and the cover plates is usually re...
Current FAA regulations limit the speed of civilian passenger jets to subsonic or transonic speeds d...
New design goals on modern jet engines often leads to more highly loaded turbines with fewer stages ...
New design goals on modern jet engines often leads to more highly loaded turbines with fewer stages ...
This paper presents experiments and CFD calculations of a Low Pressure Turbine/Outlet Guide Vane (LP...
To obtain validation for an aerodynamically loaded guide vane in a turbine duct, a new configuration...
This paper presents experiments and CFD calculations of a Low Pressure Turbine/Outlet Guide Vane (LP...
A flow control study was initiated upon a generic submerged inlet to determine whether discrete blow...
Due to the large disturbance created by the sonic boom, supersonic flight is strictly controlled by ...
This paper describes an experiment carried out in a model of an inlet system containing a plenum cha...
To improve the flow characteristics of diesel engines with twin intake ports, this study evaluates t...
As ke Thorlund for valuable comments on the design of guide vanes. We are grateful to Mr. Ulf Landé...
Various experimental and numerical studies of advanced blade configurations for variable inlet guide...
The article describes the research on the intake manifold for ultralight aircraft engine Vaxell 100i...
An investigation of the flow fields of mesoscale inlet guide vanes is presented in this paper. An in...
In Francis turbine, a small clearance gap between the guide vanes and the cover plates is usually re...
Current FAA regulations limit the speed of civilian passenger jets to subsonic or transonic speeds d...
New design goals on modern jet engines often leads to more highly loaded turbines with fewer stages ...
New design goals on modern jet engines often leads to more highly loaded turbines with fewer stages ...
This paper presents experiments and CFD calculations of a Low Pressure Turbine/Outlet Guide Vane (LP...
To obtain validation for an aerodynamically loaded guide vane in a turbine duct, a new configuration...
This paper presents experiments and CFD calculations of a Low Pressure Turbine/Outlet Guide Vane (LP...
A flow control study was initiated upon a generic submerged inlet to determine whether discrete blow...
Due to the large disturbance created by the sonic boom, supersonic flight is strictly controlled by ...
This paper describes an experiment carried out in a model of an inlet system containing a plenum cha...
To improve the flow characteristics of diesel engines with twin intake ports, this study evaluates t...
As ke Thorlund for valuable comments on the design of guide vanes. We are grateful to Mr. Ulf Landé...
Various experimental and numerical studies of advanced blade configurations for variable inlet guide...
The article describes the research on the intake manifold for ultralight aircraft engine Vaxell 100i...