Analysis of active cooling panels in a scramjet combustor considering the thermal cracking of hydrocarbon fuel-Reference-Cited by-同舟云学术

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Analysis of active cooling panels in a scramjet combustor considering the thermal cracking of hydrocarbon fuel

Published:2019-01 Issue: Volume:147 Page:231-241
ISSN:1359-4311
Container-title:Applied Thermal Engineering
language:en
Short-container-title:Applied Thermal Engineering

Author:

Sreekireddy Pavani,Reddy Tadisina Kishen Kumar^ORCID,Selvaraj Prabhu,Reddy Vanteru Mahendra,Lee Bok Jik

Funder

Defense Research Development Laboratory

Advanced Research Center

Basic Science Research

National Research Foundation of Korea

Publisher

Elsevier BV

Subject

Industrial and Manufacturing Engineering,Energy Engineering and Power Technology

Reference38 articles.

1. Design of a convective cooling system for a mach 6 hypersonic transport airframe;Helenbrook;NASA,1971

2. Internal convective cooling systems for hypersonic aircraft;Anthony;NASA,1975

3. Liquid fuels and propellants for aerospace propulsion: 1903–2003;Edwards;J. Propul. Power,2003

4. Materials property profiles for actively cooled panels: an illustration for Scramjet applications;Vermaak;Metal. Mater. Trans. A,2009

5. Liquid hydrocarbon fuels for hypersonic propulsion;Maurice;Scramjet propul. Prog. Astronaut. Aeronaut.,2001

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