2022
DOI: 10.1063/5.0087526
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Oscillation of the shock train under synchronous variation of incoming Mach number and backpressure

Abstract: Experiments were conducted to characterize shock train oscillation under the simultaneous variation of the incoming Mach number and backpressure. Under steady and low-frequency oscillatory backpressure (2 Hz), the incoming Mach number varied from 1.8 to 2.4. According to the intersection of downgoing background wave with bottom front leg, Mach stem, and top front leg of the normal shock train leading edge, the normal shock train/background wave interaction can be divided into three types. Two types of oblique … Show more

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Cited by 25 publications
(1 citation statement)
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“…In fact, the incident shock stemming from the inlet lip can create a series of shock waves and expansion waves even in straight isolators and change the shock-train characteristics, which has been a research focus for the past decades. [11][12][13][14][15] One subtopic that attracted attention is the kinematic and dynamic characteristics of a shock train affected by background shocks. As for this problem, Tan et al 16 first carried out a study and found that the pointing direction of leading shocks switched upwards and downwards repeatedly during the upstream propagation of the shock train.…”
Section: Literature Reviewmentioning
confidence: 99%
“…In fact, the incident shock stemming from the inlet lip can create a series of shock waves and expansion waves even in straight isolators and change the shock-train characteristics, which has been a research focus for the past decades. [11][12][13][14][15] One subtopic that attracted attention is the kinematic and dynamic characteristics of a shock train affected by background shocks. As for this problem, Tan et al 16 first carried out a study and found that the pointing direction of leading shocks switched upwards and downwards repeatedly during the upstream propagation of the shock train.…”
Section: Literature Reviewmentioning
confidence: 99%