Effect of nozzle shapes on the performance of continuously rotating detonation engine

Effect of nozzle shapes on the performance of continuously rotating detonation engine

48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition

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Bibliographic Details
Main Authors: Yi, T.-H., Lou, J., Turangan, C., Khoo, B.C., Wolanski, P.
Other Authors: MECHANICAL ENGINEERING
Format: Conference or Workshop Item
Published: 2014
Online Access:http://scholarbank.nus.edu.sg/handle/10635/73393
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Institution: National University of Singapore
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Summary:48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition

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