Effects of combustion on supersonic film cooling using gaseous hydrocarbon fuel as coolant

Author:

Zuo Jingying,Zhang Silong,Wei Dingyuan,Meng Linghui,Qin Jiang,Bao Wen,Haidn Oskar J.

Funder

National Natural Science Foundation of China

National Postdoctoral Program for Innovative Talents

China Postdoctoral Science Foundation

Shenzhen Technology Projects

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference30 articles.

1. Multi-objective optimization of round-to-slot film cooling holes on a flat surface;Huang;Aerosp. Sci. Technol.,2020

2. Effects of angled film-cooling on cooling performance in a GO2/GH2 subscale thrust chamber;Xiang;Appl. Therm. Eng.,2019

3. Investigation of flow characteristics inside a dual bell nozzle with and without film cooling;Verma;Aerosp. Sci. Technol.,2020

4. Experimental investigation of isoenergetic film-cooling flows with shock interaction;Marquardt;AIAA J.,2019

5. Flame characteristics in supersonic combustor with hydrogen injection upstream of cavity flameholder;Sun;J. Propuls. Power,2008

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