Numerical study on spray characteristics of liquid jets in supersonic crossflow
Author:
Funder
National Natural Science Foundation of China
Hunan Provincial Innovation Foundation for Postgraduate
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference50 articles.
1. Research progress on strut-equipped supersonic combustors for scramjet application;Chang;Prog. Aerosp. Sci.,2018
2. An analytical theory of heated duct flows in supersonic combustors;Wu;Theor. Appl. Mech. Lett.,2014
3. Numerical investigation of mode transition and hysteresis in a cavity-based dual-mode scramjet combustor;Zhang;Aerosp. Sci. Technol.,2019
4. Investigations on flame liftoff characteristics in liquid-kerosene fueled supersonic combustor equipped with thin strut;Zhang;Aerosp. Sci. Technol.,2019
5. Scaling effects on combustion modes in a single-side expansion kerosene-fueled scramjet combustor;Li;Chin. J. Aeronaut.,2021
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