FEASIBLE OPTIMUM DESIGN OF A TURBOCOMPOUND DIESEL BRAYTON CYCLE FOR DIESEL-TURBO-FAN AIRCRAFT PROPULSION

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Veröffentlicht in:Heat and Technology 2012-12, Vol.30 (2), p.121-126
Hauptverfasser: Piancastelli, L., Frizziero, L., Rocchi, I.
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title FEASIBLE OPTIMUM DESIGN OF A TURBOCOMPOUND DIESEL BRAYTON CYCLE FOR DIESEL-TURBO-FAN AIRCRAFT PROPULSION
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