TY - GEN
T1 - Investigation of the self-starting ability of an internal waverider inlet for ramjet
AU - Zuo, Fengyuan
AU - Huang, Guoping
AU - Xia, Chen
AU - Tang, Weiyuan
N1 - Publisher Copyright:
© 2015, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2015
Y1 - 2015
N2 - The Internal WaveRider Inlet (IWRI) is a new type of 3D inward turning inlet with rather good performance. It still has a difficulty, no enough good self-starting ability, when IWRI used as a geometry-fixed inlet for ramjets. At first, this research presented a theoretical analysis method of starting ability and self-starting ability for IWRI, to prove that the IWRI applied in ramjet was facing more difficult challenges of self-starting ability than scramjet. The self-starting ability should be considered in the process of designing ramjet inlet. Then, effects of bleeding mechanism on geometry-fixed ramjet IWRI was investigated by flow numerical simulation, and numerical results shown that IWRI’s self-starting ability at low Mach numbers was improved obviously: lowest Mach number of self-starting was decreased from 3.8 to 3.2, which also can endure the greater compression ratio of 32 than 28 with no bleeding. Two different groups of bleeding positions indicated that bleeding before throat section has no effect on the self-starting ability of IWRI.
AB - The Internal WaveRider Inlet (IWRI) is a new type of 3D inward turning inlet with rather good performance. It still has a difficulty, no enough good self-starting ability, when IWRI used as a geometry-fixed inlet for ramjets. At first, this research presented a theoretical analysis method of starting ability and self-starting ability for IWRI, to prove that the IWRI applied in ramjet was facing more difficult challenges of self-starting ability than scramjet. The self-starting ability should be considered in the process of designing ramjet inlet. Then, effects of bleeding mechanism on geometry-fixed ramjet IWRI was investigated by flow numerical simulation, and numerical results shown that IWRI’s self-starting ability at low Mach numbers was improved obviously: lowest Mach number of self-starting was decreased from 3.8 to 3.2, which also can endure the greater compression ratio of 32 than 28 with no bleeding. Two different groups of bleeding positions indicated that bleeding before throat section has no effect on the self-starting ability of IWRI.
UR - https://www.scopus.com/pages/publications/85088063730
U2 - 10.2514/6.2015-3748
DO - 10.2514/6.2015-3748
M3 - 会议稿件
AN - SCOPUS:85088063730
SN - 9781624103216
T3 - 51st AIAA/SAE/ASEE Joint Propulsion Conference
BT - 51st AIAA/SAE/ASEE Joint Propulsion Conference
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - 51st AIAA/SAE/ASEE Joint Propulsion Conference, 2015
Y2 - 27 July 2015 through 29 July 2015
ER -