1992
DOI: 10.1115/1.2906658
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Wave Engine Aerothermodynamic Design

Abstract: A method for aerothermodynamic preliminary design of a wave engine is presented. The engine has a centrifugal precompressor for the wave rotor, which feeds high and low-pressure turbines. Three specific wave engine designs are presented. Wave rotor blades are naturally cooled by the ingested air; thus combustion temperatures can be as high as 1900 K. Engine pressure ratios of over 25 are obtained in compact designs. It is shown that placing no nozzles at the end of the rotor blade passages yields the highest c… Show more

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Cited by 4 publications
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“…Again energy exchangers turn out to be a favorable concept. Weber (1992) also predicts high cycle efficiencies for wave engines with low precompression ratios.…”
Section: Introductionmentioning
confidence: 87%
“…Again energy exchangers turn out to be a favorable concept. Weber (1992) also predicts high cycle efficiencies for wave engines with low precompression ratios.…”
Section: Introductionmentioning
confidence: 87%