Combustion dynamics of high Mach number scramjet under different inflow thermal nonequilibrium conditions

Author:

Ao YuORCID,Wu KunORCID,Lu Hongbo,Ji Feng,Fan Xuejun

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference49 articles.

1. A brief review on the recent advancement in the field of jet engine - scramjet engine;Das;Mater. Today: Proc.,2021

2. A Review of Reaction Rates and Thermodynamics and Transport Properties for the 11-Species Air Model for Chemical and Thermal Nonequilibrium Calculations to 30000K, NASA Report 1232;Gupta,1990

3. Computational investigation of thermal nonequilibrium effects in scramjet geometries;Gehre;J. Propul. Power,2013

4. An open-source hypersonic solver for non-equilibrium flows;Vatansever;J. Aeronaut. Sp. Technol.,2021

5. A two-temperature open-source CFD model for hypersonic reacting flows, part two: multi-dimensional analysis;Casseau;Aerospace,2016

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