Design of an airworthy turboshaft engine quick-start system with compact pressurized air supply for rotorcraft application

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dc.contributor.author Kerler, M.
dc.contributor.author Schäffer, C.
dc.contributor.author Erhard, W.
dc.contributor.author Gümmer, V.
dc.date.accessioned 2018-10-22T08:26:03Z
dc.date.available 2018-10-22T08:26:03Z
dc.date.issued 2016
dc.identifier.other ERF2016_118_M. KERLER _P
dc.identifier.uri http://hdl.handle.net/20.500.11881/3735
dc.language.iso en
dc.subject.other Engines & Propulsion
dc.title Design of an airworthy turboshaft engine quick-start system with compact pressurized air supply for rotorcraft application
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