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

Thumbnail Image

Files

ERF2016_118_M. KERLER _P.pdf (973.86 KB)

Date

2016

Authors

Journal Title

Journal ISSN

Volume Title

Publisher

Abstract

Description

Keywords

Citation

URI

http://hdl.handle.net/20.500.11881/3735

Collections

Papers

Endorsement

Review

Supplemented By

Referenced By