Numerical Analysis of Thermochemical Nonequilibrium Flows in a Model Scramjet Engine

Numerical Analysis of Thermochemical Nonequilibrium Flows in a Model Scramjet Engine

This numerical study was conducted to investigate the flow properties in a model scramjet configuration of the experiment in the T4 shock tunnel. In most numerical simulations of flows in shock tunnels, the inflow conditions in the test section are determined by assuming the thermal equilibrium of t...

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Bibliographic Details
Main Authors: Seoeum Han, Sangyoon Lee, Bok Jik Lee
Format: Article
Language:English
Published: MDPI AG 2020-01-01
Series:Energies
Subjects:
scramjet engine
thermochemical nonequilibrium
hypersonic flow
shock tunnel
Online Access:https://www.mdpi.com/1996-1073/13/3/606

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https://www.mdpi.com/1996-1073/13/3/606

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