Physical models
Airbreathing Engine Combustors. Part 2: Modeling and Numerical Simulation
Article REF: TRP4012 V1
Physical models
Airbreathing Engine Combustors. Part 2: Modeling and Numerical Simulation

Author : Nicolas Bertier

Publication date: October 10, 2025 | Lire en français

Logo Techniques de l'Ingenieur You do not have access to this resource.
Request your free trial access! Free trial

Already subscribed?

1. Physical models

1.1 Equations of aerothermochemistry

The equations solved for reactive flows in aircraft combustion chambers are those of aerothermochemistry. These are essentially the Navier-Stokes equations used in fluid mechanics (see, for example, or

You do not have access to this resource.
Logo Techniques de l'Ingenieur

Exclusive to subscribers. 97% yet to be discovered!

You do not have access to this resource. Click here to request your free trial access!

Already subscribed?

Article included in this offer

"Hydraulic, aerodynamic and thermal machines"

( 177 articles )

Complete knowledge base

Updated and enriched with articles validated by our scientific committees

Services

A set of exclusive tools to complement the resources

View offer details
Contact our team FAQ