Published January 2008
| public
Book Section - Chapter
Numerical Study of Detonation Interaction with a Single-Stage Axial Turbine
Chicago
Abstract
In the present paper, we examine a single two-dimensional detonation wave propagating in a single-stage axial flow turbine. The objective or this study is the computation of the detailed now field and estimating the turbine work output. Turbine extracted work for a single operation is evaluated by energy balance and mechanical approaches. Adiabatic efficiencies at the rotor obtained by energy balance predict 50 to 70% and shows good agreement with the efficiencies by mechanic.al approach, depending on the rotor speed.
Additional Information
© 2008 by the American Institute of Aeronautics and Astronautics, Inc. Published online: 19 June 2012.Additional details
- Eprint ID
- 100982
- Resolver ID
- CaltechAUTHORS:20200129-081539732
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2020-01-29Created from EPrint's datestamp field
- Updated
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2021-11-16Created from EPrint's last_modified field
- Caltech groups
- GALCIT
- Other Numbering System Name
- AIAA Paper
- Other Numbering System Identifier
- 2008-985