SimScale logo
Set up your own cloud-native simulation in minutes.Start Simulating Now

Convergent-Divergent Nozzle

Open Project
Copy Project
views 186shares 0
jagatheaswaran
jagatheaswaran
Created

Last modified

Statistics
geometries 0 Geometriesmeshes 0 Meshessimulations 0 Simulation setupsruns 0 Results
About this project

To analysis the flow of air in a convergent-divergent nozzle, with the inlet Mach number as 0.5

Share this project

Related Projects

airflow_around_a_spoiler_1 image
Tutorial - Airflow around a spoiler

by Ali_ArafatAli_Arafat

tutorial-_harmonics_analysis_of_an_airfoil_-2-2-_3 image
Tutorial: Harmonics Analysis of an Airfoil (2/2)

by simscalesimscale

tutorial-_compressible_flow_around_a_wing image
Tutorial: Compressible Flow Around a Wing

by simscalesimscale

airplane_cabin_fluid_flow_simulation image
Fluid Flow Simulation of an Airplane Cabin Ventilation

by jprobstjprobst

proyecto_simscale image
Drone LM RQ-170 Sentinel CFD - Drag Coefficient

by robertpmrobertpm

Project History

  • jagatheaswaran

    jagatheaswaran created this project