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Studies of Shock Wave Reflections and Interactions (Paul Vieille Lecture) Read chapter Read first chapter

2017 | OriginalPaper | Chapter

Study of Cluster Linear Plug Nozzle Flow Field in Freestream Flow

Authors : M. Viji, Kiran Chutkey, S. B. Verma

Published in: 30th International Symposium on Shock Waves 1

Publisher: Springer International Publishing

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Abstract

Experiments were carried out to understand the flow field development from a cluster linear plug nozzle. The flow field was studied with the internal nozzle operating at both overexpanded and underexpanded condition in the absence and presence of freestream flow. For all the conditions tested, jets from each of the cluster module seem to interact with each other depending on the module flow expansion condition resulting in a complex three-dimensional flow field development. These three-dimensional flow features were studied using static pressure measurements on the plug and surface oil flow visualization.

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previous chapter Mixing Enhancement in Free Jets from Supersonic ESTS Lobed Nozzles
next chapter Studies in Free Jets from Supersonic ESTS Lobed Nozzles
Literature
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Hagemann, G., Immich, H., Nguyen, T.V., Dumnov, G.E.: Advanced rocket nozzles. J. Propuls. Power 14(5), 620–634 (1998)CrossRef
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Tomita, T., Tamura, H., Takahashi, M.: An experimental evaluation of plug nozzle flow field. AIAA paper, 2632, 1996
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Nasuti, F., Onofri, M.: Theoretical analysis and engineering modeling of flowfields in clustered module plug nozzles. J. Propuls Power 15(4), 544–551 (1999)
4.
Verma, S.B., Viji, M.: Linear-plug flow field and base pressure development in freestream flow. J. Propuls. Power 27(6), 1247–1258 (2011)CrossRef
5.
Tsutsumi, S., et al.: Clustering effects on performance and heating of a linear Aerospike nozzle. AIAA Paper 122-2007. 2007
Metadata
Title
Study of Cluster Linear Plug Nozzle Flow Field in Freestream Flow
Authors
M. Viji
Kiran Chutkey
S. B. Verma
Copyright Year
2017
Book
30th International Symposium on Shock Waves 1

Print ISBN: 978-3-319-46211-0

Electronic ISBN: 978-3-319-46213-4

Copyright Year: 2017

DOI
https://doi.org/10.1007/978-3-319-46213-4_16

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