Gas Dynamics

Flow relations, such as isentropic, normal shock, Rayleigh, Fanno, and Prandtl-Meyer

Calculate flow relations for Fanno lines, isentropic, normal shock, Prandtl-Meyer functions, and Rayleigh lines. When possible, these functions assume perfect gas environments. Each function has an mtype argument that lets you specify the inputs for the flow.

Functions

`flowfanno`	Fanno line flow relations
`flowisentropic`	Isentropic flow ratios
`flownormalshock`	Normal shock relations
`flowprandtlmeyer`	Calculate Prandtl-Meyer functions for expansion waves
`flowrayleigh`	Rayleigh line flow relations

Featured Examples

Calculating Compressor Power Required in a Supersonic Wind Tunnel

Calculating Compressor Power Required in a Supersonic Wind Tunnel

Calculate the required compressor power in a supersonic wind tunnel.

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Analyzing Flow with Friction Through an Insulated Constant Area Duct

Analyzing Flow with Friction Through an Insulated Constant Area Duct

Implement a steady, viscous flow through an insulated, constant-area duct using Aerospace Toolbox software. This flow is also called Fanno line flow.

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Determine Heat Transfer and Mass Flow Rate in a Ramjet Combustion Chamber

Determine Heat Transfer and Mass Flow Rate in a Ramjet Combustion Chamber

Determine heat transfer and mass flow rate in a ramjet combustion chamber.

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Solving for the Exit Flow of a Supersonic Nozzle

Solving for the Exit Flow of a Supersonic Nozzle

Use the method of characteristics and Prandtl-Meyer flow theory to solve a problem in supersonic flow involving expansions.

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