PRELIMINARY PERFORMANCE ANALYSIS OF THE PULSE-DETONATION-JET ENGINE SYSTEM

An engine capable of propelling a guided missile from zero flight speed to a cruising Mach number of 2.80 was assumed. The detonation tubes are arranged in 6 concentric rows of 32 tubes each, which gives an engine diameter of 34 in. The length of the tubes is 15 in., and the over-all length of the e...

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Bibliographische Detailangaben
1. Verfasser:	Bitondo, D
Format:	Report
Sprache:	eng
Schlagworte:	ASSEMBLY BORIDES CYCLES DETONATION WAVES FUEL AIR RATIO FUEL CONSUMPTION GRAPHITE GUIDED MISSILES Jet and Gas Turbine Engines LENGTH LOW RATE MACH NUMBER PULSE COMPRESSION PULSEJET ENGINES SHOCK WAVES STATIC TESTS TEMPERATURE THRUST TUBES ZIRCONIUM
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