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Optimum location of pressure measurements around a wing as a dynamic control input in smooth and turbulent conditions

conference contribution
posted on 2024-10-31, 17:46 authored by Sridhar RaviSridhar Ravi, Matthew MarinoMatthew Marino, Simon WatkinsSimon Watkins
Transient pressures occurring at different chordwise locations were compared with the transient lift generated by a NACA2313 wing subjected to smooth and turbulent flows. Pressures close to the leading-edge correlated well with lift fluctuations and the presence of a linear relationship between local pressure and integrated lift was also identified.

History

Related Materials

  1. 1.
    ISBN - Is published in 9780956533319 (urn:isbn:9780956533319)
  2. 2.
    URL - Is published in http://www.icas.org/ICAS_ARCHIVE/ICAS2012/PAPERS/972.PDF

Start page

1

End page

8

Total pages

8

Outlet

28th Congress of the International Council of the Aeronautical Sciences

Name of conference

28th Congress of the International Council of the Aeronautical Sciences

Publisher

ICAC

Place published

Brisbane, Australia

Start date

2012-09-23

End date

2012-09-28

Language

English

Copyright

© 2012 ICAC

Former Identifier

2006047989

Esploro creation date

2020-06-22

Fedora creation date

2015-01-14

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    Scholarly Works

    Categories

    Keywords

    dynamic controlpressure measurementssmooth flowturbulent flowwing

    Licence

    All rights reserved

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