Isolator characteristics under steady and oscillatory back pressures

被引:23
作者
Saravanan, R. [1 ,2 ]
Desikan, S. L. N. [1 ]
Muruganandam, T. M. [2 ]
机构
[1] Vikram Sarabhai Space Ctr, Wind Tunnel Data Div, Aeronaut Ent, Thiruvananthapuram 695022, Kerala, India
[2] Indian Inst Technol Madras, Dept Aerosp Engn, Chennai 600036, Tamil Nadu, India
关键词
SHOCK-TRAIN; UNSTART; MODEL; BACKPRESSURE; FLOW;
D O I
10.1063/5.0016360
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
Experiments are carried out to characterize the un-start/re-start phenomena in an isolator with steady and low-frequency oscillatory back pressures (0.75 Hz-2.5 Hz) in Mach 1.7 flow. In the present study, the effect of shock train interaction with the intake shocks is focused to capture these phenomena. It is demonstrated that the un-start mechanism is a continuous process with steady back pressures, whereas it is a discontinuous process under oscillatory back pressures. The un-start mechanism is triggered once the oscillatory back pressure is above the maximum isolator pressure. As the frequency of back pressure oscillation is increased, the isolator experiences an early un-start and a delayed re-start. On the other hand, if the oscillatory back pressure is decreased, the re-start process is initiated. During the re-start process, the time lag is found to be increased, and the hysteresis loss is decreased with an increase in oscillatory frequencies. These phenomena are studied through both the steady and unsteady pressure measurements along with instantaneous schlieren images for different dynamic pressures. Furthermore, the un-start can be avoided or delayed by increasing the freestream dynamic pressure. Published under license by AIP Publishing.
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页数:12
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