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

2017 | OriginalPaper | Chapter

Design and Validation of an Uncooled Pitot Probe for Hot, Supersonic Flow Investigations

Authors : Felix J. Förster, Nils C. Dröske, Jens von Wolfersdorf, Bernhard Weigand

Published in: 30th International Symposium on Shock Waves 1

Publisher: Springer International Publishing

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Abstract

A detailed understanding of supersonic free jets and the underlying flow phenomena is key to many technical applications such as exhaust nozzle flows of aircraft or rocket engines, or for well-defined test cases in the validation process of numerical setups. In this paper, we suggest an uncooled, low-cost pitot probe made from a high perfomance metall alloy. The paper describes the design of the probe, the obstacles during the manufacturing process and presents validation and application cases for free jets with an inlet total temperature of up to 1100K.

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previous chapter Overexpanded Jet Flow Theoretical Analysis in the Vicinity of the Nozzle Lip
next chapter Large Eddy Simulation of a Supersonic Underexpanded Square Jet
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Metadata
Title
Design and Validation of an Uncooled Pitot Probe for Hot, Supersonic Flow Investigations
Authors
Felix J. Förster
Nils C. Dröske
Jens von Wolfersdorf
Bernhard Weigand
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_49

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