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

Nango, Ayaka and Inaba, Kazuaki and Kojima, Takayuki and Yamamoto, Makoto (2008) Numerical Study of Detonation Interaction with a Single-Stage Axial Turbine. In: 46th AIAA Aerospace Sciences Meeting and Exhibit. American Institute of Aeronautics and Astronautics , Reston, VA, Art. No. 2008-985. ISBN 978-1-62410-128-1. https://resolver.caltech.edu/CaltechAUTHORS:20200129-081539732

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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.


Item Type:Book Section
Related URLs:
URLURL TypeDescription
https://doi.org/10.2514/6.2008-985DOIArticle
Additional Information:© 2008 by the American Institute of Aeronautics and Astronautics, Inc. Published online: 19 June 2012.
Group:GALCIT
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AIAA Paper2008-985
Record Number:CaltechAUTHORS:20200129-081539732
Persistent URL:https://resolver.caltech.edu/CaltechAUTHORS:20200129-081539732
Official Citation:Numerical Study of Detonation Interaction with a Single-Stage Axial Turbine. Ayaka Nango, Kazuaki Inaba, Takayuki Kojima, and Makoto Yamamoto. 46th AIAA Aerospace Sciences Meeting and Exhibit. January 2008; doi: 10.2514/6.2008-985
Usage Policy:No commercial reproduction, distribution, display or performance rights in this work are provided.
ID Code:100982
Collection:CaltechAUTHORS
Deposited By: Tony Diaz
Deposited On:29 Jan 2020 17:09
Last Modified:29 Jan 2020 17:09

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