Investigation of Vaporized Kerosene Injection in a Supersonic Model Combustor


Autoria(s): Yu G(俞刚); Li JG(李建国); Zhao Z; Zhang XY(张新宇); Sun CJ
Data(s)

2003

Resumo

Characteristics of vaporized aviation kerosene injection in a supersonic model combustor were preliminarily investigated. The electrically storage type heater has a volume capacity of heating kerosene of 0.8 kg up to 670 K at a pressure of 5.5 Mpa. The temperature to cause pressurized kerosene jet being fully vaporized in Quiescent atmosphere was found to be 550 K at 4 Mpa however the pressurized hot kerosene remains in liquid state within the tube. The correspondent jet spray in Mach 2.5 vitiated air cross-flow were visualized by using stop schlieren photograph.It was found the penetration depth of the hot pressurized kerosene jet is approximately same with the temperature varied from 290 K to 550 k. at pressure of 4 Mpa. This results showed that the atomization process of hot kerosene jet spray in supersonic combustor could be bypassed and directly transferred to be gas state at temperature 550 K and pressure of 4 Mpa.

Identificador

http://dspace.imech.ac.cn/handle/311007/13796

http://www.irgrid.ac.cn/handle/1471x/6610

Idioma(s)

英语

Fonte

Asian Joint Conference on Propulsion and Power,2004

Palavras-Chave #力学
Tipo

会议论文