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 |
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container_issue | 2 |
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container_title | Heat and Technology |
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creator | Piancastelli, L. Frizziero, L. Rocchi, I. |
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doi_str_mv | 10.18280/ijht.300217 |
format | Article |
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source | Elektronische Zeitschriftenbibliothek - Frei zugängliche E-Journals |
title | FEASIBLE OPTIMUM DESIGN OF A TURBOCOMPOUND DIESEL BRAYTON CYCLE FOR DIESEL-TURBO-FAN AIRCRAFT PROPULSION |
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