Experimental investigation on combustion performance of cavity-strut injection of supercritical kerosene in supersonic model combustor

Author:

Sun Ming-bo,Zhong Zhan,Liang Jian-han,Wang Hong-bo

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference13 articles.

1. Combustion and ignition of thermal cracked kerosene in supersonic model combustors;Fan;J. Propuls. Power,2007

2. Performance of Supersonic Model Combustors with Distributed Injection of Supercritical Kerosene;Fan,2007

3. Performance of a dual-mode combustor with multistaged fuel injection;Kobayashi;J. Propuls. Power,2006

4. K. Cabell, N. Hass, A. Storch, M. Gruber. HIFiRE Direct-Connect Rig (HDCR) Phase I Scramjet Test Results from the NASA Langley Arc-Heated Scramjet Test Facility. AIAA paper 2011–2248, 2011

5. M.R. Gruber. Fundamental Investigations of an Integrated Fuel Injector/Flameholder Concept for Supersonic Combustion. AFRL-PR-WP-TR-1998-2111, 1998

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