Published January 2008 | Version public
Book Section - Chapter

Numerical Study of Detonation Interaction with a Single-Stage Axial Turbine

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

Identifiers

Eprint ID
100982
Resolver ID
CaltechAUTHORS:20200129-081539732

Dates

Created
2020-01-29
Created from EPrint's datestamp field
Updated
2021-11-16
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Caltech Custom Metadata

Caltech groups
GALCIT
Other Numbering System Name
AIAA Paper
Other Numbering System Identifier
2008-985