Oscillating Flows in a Model Pulse Detonation Engine Inlet

A supersonic inlet with backpressure excitation to simulate the flowfield experienced by the inlet of a pulse detonation engine was tested at Mach 2.5. The excitation was varied from 15 to 50 Hz, and increasing the blockage at the exit plane varied the amplitude. Flow visualization using schlieren a...

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Veröffentlicht in:	AIAA journal 2003-02, Vol.41 (2), p.324-326
Hauptverfasser:	Mullagiri, S, Segal, C, Hubner, P. J
Format:	Artikel
Sprache:	eng
Schlagworte:	Applied sciences Energy Energy. Thermal use of fuels Engines and turbines Equipments for energy generation and conversion: thermal, electrical, mechanical energy, etc Exact sciences and technology
Online-Zugang:	Volltext
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