Compressible

Find projects using the compressible analysis type here. | Page 195

This is just a copy to see the streamlines of a Paper Plane

This project is intended to investigate the different drag characteristics of versions of fins intended for a model rocket using the Prandtl-D tip  (NASA Preliminary Research Aerodynamic Design To Lower Drag) airfoil profile. The primary intent is to determine whether drag characteristics are improved or detracted by the truncation of the fin profile through the limitation of max thickness of the fin.

The type of turbine was first appear at Seventeen century. At 1368 to 1644 AC,  it was being regularly used by farmers of Jiangsu city.

Design an intake manifold for the four cylinders with a maximum length of 1.5 m and a maximum pressure loss from the start to the entry of the last 250 Pa cylinder. Adjust the design according to the results with the SimScale.

Analizar el comportamiento del colector y el tubo de escape

Analizar el comportamiento de un tubo de escape

Analizar el flujo de gases en el tubo de escape

Analisis del flujo de aire por la parte inferior del coche para generar carga aerodinámica

It is a simple test to compute de free surface that a cylinder generates

CFD Analysis of the model of the undertray of a Ferrari 458 with scale 1/50

Practice to learn more about post processing and aerodynamics

We will simulate the generation if a normal shock wave in a de Laval nozzle. A shock wave occurs when supersonic flow can not maintain the regime anymore when the pressure downstrem is too high. To match the outside pressure, an non isentropic process happens in which the fluid properties change suddenly. In the case we will be studying, a nozzle expands air below 0,1 bar when the outside pressure is 1 bar, so a normal shock wave occurs.

Compressible | SimScale Project Library | Page 195