What is free stream flow?
Continuous lines are free air stream airflow. The air in a region where pressure, temperature, and relative velocity are unaffected by the passage of aircraft through it. Also known as relative airflow (RAF).
What are free stream conditions?
The freestream is the air far upstream of an aerodynamic body, that is, before the body has a chance to deflect, slow down or compress the air. Freestream conditions are usually denoted with a symbol, e.g. , meaning the freestream velocity.
What is free stream pressure?
The free stream total pressure (P0) is a function of both pressure altitude and flight Mach number. Free stream total temperature (T0) is a function also of ambient temperature and flight Mach number. Both inlet pressure and temperature are fundamental to engine performance.
What is free stream turbulence?
With free-stream turbulence, improved fluid mixing occurs in boundary layers with adverse pressure gradients relative to the zero pressure gradient condition, with the same free-stream turbulence intensity and length scale.
What is a free stream temperature?
The free stream temperature of your problem is the temperature of that fluid which is acting as the sink. For example, in the case of a utility boiler, the free stream temperature can be defined as the mean temp of the water/steam mixture rising in the wall tubes (away from the boundary layer).
How is free stream velocity calculated?
FreeStream Velocity Definitions The boundary layer thickness is defined as the distance between the blade surface and the location where the velocity is 99.5% of the velocity of the adjacent data point: dU/dn=0.005⇒Un−1=0.995Un, where n is the normal to the blade surface.
What is free stream temperature?
What is freestream turbulence intensity?
The free-stream turbulence intensity was computed as the root-mean-square of the velocity fluctuations in the low-pass filtered signal, normalized by the mean free-stream velocity.
What is the effect of free stream velocity on thickness of boundary layer?
As the relative velocity decreases in the axial part of the compressor, the constant value of freestream velocity results in increasing boundary layer thickness until the flow direction changes from axial to radial.
What is FreeStream static pressure?
Total Pressure (2) • For fluids in motion the term static pressure is still applicable. (in particular with regard to external flows), and refers strictly to. the pressure in the fluid far upstream (freestream) of any object immersed into it. •Freestream Pressure = Ambient pressure for atmospheric flight.
What is turbulent viscosity ratio?
Turbulent viscosity ratio is defined as the ratio of turbulent viscosity to dynamic viscosity and might exceed the specified limit in highly turbulent flows (which in your case is true). So basically it is not an error.
What is turbulent viscosity?
The turbulent or eddy viscosity μt is defined by the following relationship: (2) є The field distribution of the turbulence kinetic energy k and its dissipation rate є (a measure of turbulence length scale) are obtained from the solution of the relevent transport equations.
What is Flightstream?
An aerodynamics tool for modeling and analyzing aircraft, propellers, high-lift devices and jet engine effects. FlightStream ® is a high fidelity aerodynamics tool perfectly suited for aircraft designers. The integrated meshing tool allows users to easily apply a surface mesh to their CAD models.
What is the function of flow solver in flight stream?
The solver is capable of modeling and analyzing aircraft, propellers, high-lift devices and jet engine effects. The intuitive user interface, utility of the meshing tool and robustness of the flow solver allow users of all skill levels to quickly and easily obtain accurate aerodynamic results. How does FlightStream® handle CAD geometry?
Which CAD software is Flightstream compatible with?
FlightStream ® is compatible with CAD software such as SolidWorks, AutoCAD, Solid Edge, CATIA, Autodesk and many more. Have a CAD model but no mesh? No problem!
What is the difference between free stream and compressed air?
At the exit of the compressor, the air is at a much higher pressure than free stream. In the burner a small amount of fuel is combined with the air and ignited. In a typical jet engine, 100 pounds of air/sec is combined with only 2 pounds of fuel/sec.