Study of a supersonic reacting wall jet with a variable turbulent Prandtl and Schmidt number approach-Reference-Cited by-同舟云学术

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Study of a supersonic reacting wall jet with a variable turbulent Prandtl and Schmidt number approach

Published:2020-11 Issue: Volume:106 Page:106070
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Hoste J.J.O.E.^ORCID,Fechter S.^ORCID,Karl S.^ORCID,Hannemann K.

Funder

DAAD

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference56 articles.

1. Status of turbulence modeling for hypersonic propulsion flowpaths;Georgiadis;Theor. Comput. Fluid Dyn.,2014

2. Supersonic combustion in air-breathing propulsion systems for hypersonic flight;Urzay;Annu. Rev. Fluid Mech.,2018

3. Modeling of High Speed Reacting Flows: Established Practices and Future Challenges;Baurle,2004

4. Role of turbulent Prandtl numbers on heat flux at hypersonic Mach numbers;Xiao;AIAA J.,2007

5. Reynolds-averaged Navier-Stokes simulations of the HyShot II scramjet;Pecnik;AIAA J.,2012

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1. A comprehensive framework for high fidelity computations of two-species compressible turbulent flows;Journal of Computational Physics;2022-08

2. Modelling of hydrogen-air supersonic mixing and combustion in near-wall region;Russian Journal of Numerical Analysis and Mathematical Modelling;2021-04-01

3. Comparison of turbulence/chemistry interaction models in the problem of ignition a parallel hydrogen jet in a supersonic air flow;AIP Conference Proceedings;2021

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