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A practical model for pressure probe system response estimation (with review of existing models)

Abstract:

The accurate estimation of the unsteady response (bandwidth) of pneumatic pressure probe systems (probe, line and transducer volume) is a common practical problem encountered in the design of aerodynamic experiments. Understanding the bandwidth of the probe system is necessary to capture unsteady flow features accurately. Where traversing probes are used, the desired traverse speed and spatial gradients in the flow dictate the minimum probe system bandwidth required to resolve the flow. Exist...

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Publication status:
Published
Peer review status:
Peer reviewed
Version:
Accepted Manuscript

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Publisher copy:
10.1088/1361-6501/aaa58f

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ORCID:
0000-0002-4725-7634
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Institution:
University of Oxford
Division:
MPLS Division
Department:
Engineering Science
Oxford college:
University College; University College; University College
Publisher:
Institute of Physics Publisher's website
Journal:
Measurement Science and Technology Journal website
Volume:
29
Issue:
4
Pages:
045301
Publication date:
2018-02-26
Acceptance date:
2018-01-05
DOI:
EISSN:
1361-6501
ISSN:
0957-0233
Pubs id:
pubs:832009
URN:
uri:27375230-a34c-4e8b-a055-cb6b41c3df5f
UUID:
uuid:27375230-a34c-4e8b-a055-cb6b41c3df5f
Local pid:
pubs:832009

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