The Design and Performance of a High Temperature Rise Combustor for Wind Tunnel

作     者：Zhang Rongchun Fan Weijun 

作者机构：National Key Laboratory on Aero-Engines School of Jet Propulsion Beijing University of Aeronautics and Astronautics Beijing 100191 China 

出 版 物：《Journal of Thermal Science》 (热科学学报（英文版）)

年 卷 期：2011年第20卷第6期

页      码：556-562页

摘      要：A high-temperature-rise combustor that can be used in high-temperature wind tunnel is introduced in this *** kerosene is used in this type of combustor,with division combustion scheme and evaporator fuel-supply device *** the performance test under atmospheric pressure,when the inlet temperature is 500K and air flow is within the range of 1.5-3.0 kg/s,the outlet temperature can be precisely regulated within the range of ***,higher uniformity of outlet temperature distribution and higher combustion efficiency can be *** the long-time working in the wind tunnel,various components of the combustor,especially the combustor liners are checked without finding any anomaly such as thermal deformation.

主 题 词：high temperature rise evaporator wind tunnel combustor aviation kerosene 

学科分类：080703[080703] 08[工学] 082402[082402] 0807[工学-电子信息类] 0824[工学-林业工程类] 

核心收录：

D　O　I：10.1007/s11630-011-0510-5

馆 藏 号：203603312...