Wall Roughness Effects on Combustion Development in Confined Supersonic Flow-Reference-Cited by-同舟云学术

Wall Roughness Effects on Combustion Development in Confined Supersonic Flow

Published:2021-01 Issue:1 Volume:37 Page:151-166
ISSN:1533-3876
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Pelletier Guillaume¹,Ferrier Marc¹,Vincent-Randonnier Axel¹,Sabelnikov Vladimir¹,Mura Arnaud²

Affiliation:

1. DMPE ONERA—University of Paris-Saclay, F-91123 Palaiseau, France

2. Ecole Nationale Supérieure de Mécanique et d’Aérotechnique, 86961 Futuroscope, France

Funder

Direction Générale de l'Armement (DGA), French Ministry of Defense

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Reference63 articles.

1. BeachH. L. “Supersonic Mixing and Combustion of a Hydrogen Jet in a Coaxial High-Temperature Test Case,” AIAA Paper 1972-1179, 1972. 10.2514/6.1972-1179

2. Raman measurement of mixing and finite-rate chemistry in a supersonic hydrogen-air diffusion flame

3. Assumed and evolution probability density functions in supersonic turbulent combustion calculations

4. Scalar and joint scalar-velocity-frequency Monte Carlo PDF simulation of supersonic combustion

5. A Lagrangian Model of Combustion in High-Speed Flows: Application to Scramjet Conditions

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