Design and Experimental Validation of a Combined PI and Bi-Positional Laws Controller for Delaying the Transition from Laminar Flow to Turbulent Flow over a Morphing Wing

Author:

Grigorie Teodor Lucian,Popov Andrei Vladimir,Botez Ruxandra Mihaela,Mamou Mahmoud,Mébarki Youssef

Publisher

Springer Berlin Heidelberg

Reference24 articles.

1. Shellabarger, N.: National Forecast Overview 2008-2025. Director Aviation Policy and Plans, Federal Aviation Administration (2008), http://www.faa.gov/news/conferences_events/aviation_forecast_2008/agenda_presentation/media/nan_shellabarger.pdf

2. Popov, A.V.: Design of an Active Controller for Delaying the Transition from Laminar Flow to Turbulent Flow over a Morphing Wing in Wind Tunnel. PhD Thesis, Ecole de Technologie Supérieure, Montréal (2009)

3. Chang, P., Shah, A., Singhee, M.: Parameterization of the Geometry of a Blended Wing Body Morphing Wing, Project report, Georgia Institute of Technology, Atlanta, Georgia, USA (April 2009)

4. Smith, K., Butt, J., Spakovsky, M.R., Moorhouse, D.: A Study of the Benefits of Using Morphing Wing Technology in Fighter Aircraft Systems. In: 39th AIAA Thermophysics Conference, Miami, Forida, USA (2007)

5. Hinshaw, T.L.: Analysis and Design of a Morphing Wing Tip using Multicellular Flexible Matrix Composite Adaptive Skins. Master of Science Thesis, Virginia Polytechnic Institute and State University, Virginia (2009)

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