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Robust aero-thermal design of high pressure turbines at uncertain exit conditions of low-emission combustion systems

Schneider, Marius (2019)
Robust aero-thermal design of high pressure turbines at uncertain exit conditions of low-emission combustion systems.
Technische Universität Darmstadt
Ph.D. Thesis, Bibliographie

Item Type: Ph.D. Thesis
Erschienen: 2019
Creators: Schneider, Marius
Type of entry: Bibliographie
Title: Robust aero-thermal design of high pressure turbines at uncertain exit conditions of low-emission combustion systems
Language: German
Referees: Schiffer, Prof. Dr. Heinz-Peter ; Hasse, Ptof. Dr. Christian
Date: 12 November 2019
Place of Publication: Düren
Publisher: Shaker
Series: Forschungsberichte aus dem Institut für Gasturbinen, Luft- und Raumfahrtantriebe
Series Volume: 13
Refereed: 17 July 2019
Divisions: 16 Department of Mechanical Engineering
16 Department of Mechanical Engineering > Institute of Gas Turbines and Aerospace Propulsion (GLR)
Date Deposited: 02 Dec 2019 08:17
Last Modified: 02 Dec 2019 08:17
PPN:
Referees: Schiffer, Prof. Dr. Heinz-Peter ; Hasse, Ptof. Dr. Christian
Refereed / Verteidigung / mdl. Prüfung: 17 July 2019
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