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In situ evaluation of terminal and in-line sensor setups for unsteady pressure measurements
KTH, School of Engineering Sciences (SCI), Aeronautical and Vehicle Engineering, Flight Dynamics.
2016 (English)Independent thesis Advanced level (degree of Master (Two Years)), 20 credits / 30 HE creditsStudent thesis
Abstract [en]

The frequency response of an in-line pressure measuring setup was investigated in order to evaluate its suitability for use in wind tunnel measurements. Testing was conducted in a laboratory environment and a general procedure was developed for both the calibration of the sensors and obtaining the transfer functions for the setup. The tests showed that the in-line setup displays a distinct frequency response, which needs to be accounted for. The developed methods were also tested as a part of a wind tunnel measurement with the calibrations and the measurement of the frequency response done on the sensors in the model, which included both terminal and in-line congurations. Finally, data for a terminal sensor obtained from the testing was corrected by using a previously measured transfer function.

Place, publisher, year, edition, pages
2016. , p. 20
Series
TRITA-AVE, ISSN 1651-7660 ; 2016:26
National Category
Engineering and Technology
Identifiers
URN: urn:nbn:se:kth:diva-198523OAI: oai:DiVA.org:kth-198523DiVA, id: diva2:1057236
Examiners
Available from: 2016-12-16 Created: 2016-12-16 Last updated: 2016-12-16Bibliographically approved

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CiteExportLink to record
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Citation style
  • apa
  • ieee
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  • de-DE
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  • en-US
  • fi-FI
  • nn-NO
  • nn-NB
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  • Other locale
More languages
Output format
  • html
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  • asciidoc
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