TY - GEN
T1 - Analysis of thermal choking in expanding RBCC duct
AU - Wu, Yake
AU - He, Guoqiang
AU - Liu, Peijin
PY - 2009
Y1 - 2009
N2 - Expanding combustor has been validated to realize the best performance of the RBCC engine which has several operating modes. But it is based on the implementation of thermal choking in the duct which was influenced by several factors including expanding angle, heating amount and heating rate etc. A theoretical one dimensional model was developed in this paper to describe the flow in an expanding duct. it is concluded by the one-dimensional analysis that the expanding angle, heating increment and heat release law are of crucial effect on the thermal choking. These factors mainly influence the position of choking throat, the total pressure loss and distribution of the temperature. In order to implement thermal choking in the duct, there must be a certain heat release law, heating increment and a special expanding angle which depends on the given heating law. In order to transit subsonic flow to supersonic flow in expanding duct, the heating rate should change from a bigger value to a smaller one.
AB - Expanding combustor has been validated to realize the best performance of the RBCC engine which has several operating modes. But it is based on the implementation of thermal choking in the duct which was influenced by several factors including expanding angle, heating amount and heating rate etc. A theoretical one dimensional model was developed in this paper to describe the flow in an expanding duct. it is concluded by the one-dimensional analysis that the expanding angle, heating increment and heat release law are of crucial effect on the thermal choking. These factors mainly influence the position of choking throat, the total pressure loss and distribution of the temperature. In order to implement thermal choking in the duct, there must be a certain heat release law, heating increment and a special expanding angle which depends on the given heating law. In order to transit subsonic flow to supersonic flow in expanding duct, the heating rate should change from a bigger value to a smaller one.
UR - http://www.scopus.com/inward/record.url?scp=77953514779&partnerID=8YFLogxK
M3 - 会议稿件
AN - SCOPUS:77953514779
SN - 9781615679089
T3 - 60th International Astronautical Congress 2009, IAC 2009
SP - 6461
EP - 6470
BT - 60th International Astronautical Congress 2009, IAC 2009
T2 - 60th International Astronautical Congress 2009, IAC 2009
Y2 - 12 October 2009 through 16 October 2009
ER -