Comparative assessment of transient characteristics of conventional and hybrid gas turbine engine

Author:

Wortmann Guido,Schmitz Oliver,Hornung Mirko

Publisher

Springer Science and Business Media LLC

Subject

Aerospace Engineering,Transportation

Reference22 articles.

1. Freeh, J.E., et al.: Hybrid solid oxide fuel cell/gas turbine system design for high altitude long endurance aerospace missions, NASA Technical Memorandum, NASA/TM-2006-214328 (2006)

2. Kuhn, H., Sizmann, A.: Fundamental prerequisities for electric flying, Deutscher Luft- und Raumfahrtkongress DLRK (2012)

3. Glassock, R., et al.: Multimodal hybrid powerplant for unmanned aerial systems (UAS) robotics, 24th Bristol International unmanned air vehicle systems conference, Bristol, UK (2009)

4. Schmitz, O., Hornung, M.: Unified applicable propulsion system performance metrics, J. Eng. Gas Turbines Power. 135(11), 1–9 (2013)

5. Schröder, D.: Elektrische Antriebe—Grundlagen, 4th edn. Springer, Dordrecht, Heidelberg, London, New York (2009)

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