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Document type:
Konferenzbeitrag / Conference Paper
Title:
Steady Performance Measurement of a Turbofan Engine with Inlet Distortions Containing Co- and Counter-Rotating Swirl from an Intake Diffuser for Hypersonic Flight
Title of conference publication:
ASME Turbo Expo 2000: Power for Land, Sea, and Air
Subtitle of conference publication:
Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery Munich, Germany, May 8–11, 2000
Organizer (entity):
ASME
Conference title:
ASME Turbo Expo (2000, München)
Venue:
München
Year of conference:
2000
Date of conference beginning:
08.05.2000
Date of conference ending:
11.05.2000
Year:
2000
Language:
Englisch
ISBN:
978-0-7918-7854-5
Article ID:
2000-GT-0011
DOI:
Department:
Fakultät für Luft- und Raumfahrttechnik
Institute:
LRT 12 - Institut für Strahlantriebe
Chair:
Niehuis, Reinhard; Fottner, Leonhard
Open Access yes or no?:
Nein / No
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