Parametric numerical analysis on the interaction between combustion and hydrocarbon fueled supersonic film cooling
Author:
Funder
National Natural Science Foundation of China
China Postdoctoral Science Foundation
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference28 articles.
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2. Parametric study of supersonic film cooling in dual bell nozzle for an experimental air–kerosene engine;Choudhury;Aerosp. Sci. Technol.,2018
3. Nozzle optimization study and measurements for a quasi-axisymmetric scramjet model;Tanimizu,2008
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5. Flame characteristics in supersonic combustor with hydrogen injection upstream of cavity flameholder;Sun;J. Propuls. Power,2008
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