1975
DOI: 10.2514/3.59818
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Investigation of the Stall Hammershock at the Engine Inlet

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Cited by 10 publications
(2 citation statements)
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“…where M is the Mach number of the ow into which the shock is travelling. 7 The upstream propagation speed…”
Section: Steady-state Resultsmentioning
confidence: 99%
“…where M is the Mach number of the ow into which the shock is travelling. 7 The upstream propagation speed…”
Section: Steady-state Resultsmentioning
confidence: 99%
“…Kurkov et al obtained static experimental measurement of the magnitude of surge-induced inlet overpressure ratio on two turbofan engines and one turbojet engine, using a broad set of engine surgeinitiation methods (9) . It was noted that different surge initiating mechanisms produce different overpressure strengths at the engine face.…”
Section: Stmentioning
confidence: 99%