Compressible Flow Simulators

Choked flow simulator for converging nozzles: analyze sonic conditions, critical pressure ratio, and maximum mass flow rate in CAE design.

Calculate Mach number and visualize compressible flow: isentropic relations, normal & oblique shocks. Adjust parameters in real-time.

Evaluate isentropic nozzle area ratio, static pressure ratio, required area, and velocity from Mach number and gas properties.

Use this page to relate representative assumptions to flow rate, pressure loss, and hydraulic margin before moving into the adjacent engineering checks.

Simulate adiabatic compressible duct flow with friction. Compute exit Mach, T and P ratios and choking length 4fL*/D on the Fanno line in real time.

Calculate isentropic, shock, Rayleigh & Fanno flow parameters in real-time. Input Mach number & specific heat ratio for compressible gas dynamics.

Calculate isentropic flow ratios and normal shock properties instantly. Input Mach number and specific heat ratio for pressure, temperature, density, and area ratios.

Jet Impact Force Simulator: Calculate the force produced when a fluid jet from a nozzle strikes a flat plate or a curved vane. Change the nozzle diameter, je…

Calculate Mach number and heat capacity ratio to instantly compute isentropic flow and normal shock conditions. Visualize subsonic to hypersonic results.

Normal Shock Relations Simulator for compressible flow analysis. Visualize Rankine-Hugoniot relations across supersonic shocks using interactive Mach number and thermodynamic property adjustments.

Calculate isentropic flow for a De Laval nozzle. Set Mach number, throat area, and stagnation conditions to instantly get pressure and temperature distributions.

Interactive isentropic nozzle flow calculator. Compute Mach number, area ratio A/A*, pressure and temperature ratios, and normal shock relations for compressible gas dynamics.

Oblique shock wave simulator using θ-β-M relation for supersonic flow analysis. Adjust Mach number, shock angle, and pressure to predict flow deflection and downstream conditions.

Prandtl-Meyer simulator: compute the turning angle, nu function, downstream pressure and temperature ratio of an isentropic supersonic expansion fan in real time.

Rayleigh Flow Simulator compares how flow rate, pressure loss, and hydraulic margin shifts as the main assumptions change.

Compute exact 1D Riemann solutions for shock tubes. Visualize pressure, density, and velocity profiles across shock waves, contact discontinuities, and rarefactions.