0
TECHNICAL PAPERS

Steady Performance Measurements of a Turbofan Engine With Inlet Distortions Containing Co- and Counterrotating Swirl From an Intake Diffuser for Hypersonic Flight

[+] Author and Article Information
Norbert R. Schmid, Dirk C. Leinhos, Leonhard Fottner

Institut für Strahlantriebe, Universität der Bundeswehr München, D-85577 Neubiberg, Germany

J. Turbomach 123(2), 379-385 (Feb 01, 2000) (7 pages) doi:10.1115/1.1343466 History: Received February 01, 2000
Copyright © 2001 by ASME
Your Session has timed out. Please sign back in to continue.

References

Figures

Grahic Jump Location
Variation of the thrust vector
Grahic Jump Location
Measured relative total pressure, cross velocities
Grahic Jump Location
Measured distortion parameters (model)
Grahic Jump Location
Distortion parameters delta wing simulator
Grahic Jump Location
LARZAC 04 C5 test engine
Grahic Jump Location
Positions of the low-frequency instrumentation
Grahic Jump Location
Relative specific fuel consumption
Grahic Jump Location
Position of the high frequency probes relative to the CO and COUNTER distortions
Grahic Jump Location
(a) CO and (b) COUNTER pressure signals near stall

Tables

Errata

Discussions

Some tools below are only available to our subscribers or users with an online account.

Related Content

Customize your page view by dragging and repositioning the boxes below.

Related Journal Articles
Related eBook Content
Topic Collections

Sorry! You do not have access to this content. For assistance or to subscribe, please contact us:

  • TELEPHONE: 1-800-843-2763 (Toll-free in the USA)
  • EMAIL: asmedigitalcollection@asme.org
Sign In