Compressible

Find projects using the compressible analysis type here. | Page 2

This project aims to find out the effect of the blended wing on the performances of the aircraft and to optimize the design of the blended wing. For this project compressible type of simulation has been chosen because the aircraft with blended wing body moves at high velocity - Copy

Checking how the input radius of the cyclone affects the circumferential velocity at the outlet - Copy

This is a case that year 3 student (2024) Ethan Nadar requested that I run for him.  Delta wing geometry with 30 degree sweep. Mach 1.6.

Étude de l'écoulement d’air autour d’un tube de Pitot - Copy - Copy

Verification model of compressible flow for pressure ratios up to 8 - Copy

Checking how the input radius of the cyclone affects the circumferential velocity at the outlet

Studies of properties of Boeing 737-800 - Copy

M2.5R Ramjet engine test (Entire engine) - Copy - Copy

Pipe flow analysis of different sized tubes at different angles in a T junction - Copy

Find where the boundary layer starts separating from the upper surface of the wing profile

Fluid dynamics simulation for Celsius-1 rocket. Thanks for the sponsorship Simscale :)

Calcultae the Interference of Dry Coolers in Turbine Air Inlet

Model air traveling across a target type thrust reverser to be used on a JetCat P100-RX. Goal is to find approximate reverse thrust and back pressure created