COMPUTATION AND ANALYSIS OF HEAT FLUX OF THE OFF-DESIGN PERFORMANCE OF SCRAMJET ON NONSTATIONARY WALL TEMPERATURE

摘要：

In order to quickly and accurately compute the wall temperature distribution along the combustor axial line, one method computing the temperature field of active regeneratively cooling combustor was adopted. On the condition of nonstationary wall temperature, the one dimensional cooling model was established first, heat transfer empirical equation is used, the wall heat flux and wall temperature distribution along the combustor axial line was obtained at different mach numbers.Afterwards as for existing two types cooling systems structure,the cooling effect of these two type cooling systems is investigated and satisfactory results was obtained.

作者: Jiang Qin Wen Bao Weixing Zhou Daren Yu

作者单位: School of Engine Science and Engineering, Harbin Institute of Technology Harbin, 150001, P.R.China

会议类型: 国际会议

会议名称: 第一届喷气推进与动力工程国际会议(Proceedings of the 1st International Symposium on Jet Propulsion and Power Engineering)

会议地点: 昆明

会议语种:英文

页码: 313-317

在线出版日期: 2006-09-18（万方平台首次上网日期，不代表论文的发表时间）