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Dr Djamel RezguiMEng, PhD

Lecturer

1 - 10 out of 35Page size: 10
  1. 2019
  2. Accepted/In press

    Nonlinear Blade Stability for a Scaled Autogyro Rotor at High Advance Ratios

    Rezgui, D. & Lowenberg, M. H., 7 Oct 2019, (Accepted/In press) American Helicopter Society, (Journal of the American Helicopter Society).

    Research output: Working paperWorking paper and Preprints

  3. Published
  4. Published

    Experimental bifurcation analysis of a wing profile

    Tartaruga, I., Barton, D. A. W., Rezgui, D. & Neild, S. A., 13 Sep 2019. 9 p.

    Research output: Contribution to conferencePaper

  5. Accepted/In press

    Resonant frequency tuning of a nonlinear helicopter inceptor model: a sensitivity analysis

    Yap, E. J. H., Rezgui, D., Lowenberg, M. H., Neild, S. A. & Rahman, K., 6 Jul 2019, (Accepted/In press) Proceedings of the 45th European Rotorcraft Forum. Warsaw, Poland, 14 p.

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

  6. Published

    Stability Analysis of Whirl Flutter in a Nonlinear Gimballed Rotor-Nacelle System

    Mair, C., Rezgui, D. & Titurus, B., 7 Jun 2019, Proceedings of the 75th Forum of the Vertical Flight Society. Philadelphia, Pennsylvania: Vertical Flight Society, p. 1-16 16 p. 389. (Annual Forum Proceedings; vol. 75).

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

  7. Published

    An Experimental Investigation of Propeller Noise in Forward Flow

    Wang, H., Celik, A., Zang, B., Rezgui, D. & Azarpeyvand, M., 20 May 2019, 25th AIAA/CEAS Aeroacoustics Conference. Delft, The Netherlands: American Institute of Aeronautics and Astronautics Inc. (AIAA), 13 p. AIAA 2019-2620

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

  8. Published

    Testing of Folding Wing-Tip for Gust Load Alleviation in High Aspect Ratio Wing

    Cheung, R., Rezgui, D., Cooper, J. & Wilson, T., 7 Jan 2019, AIAA Scitech 2019 Forum. American Institute of Aeronautics and Astronautics Inc. (AIAA), p. 1-15 15 p. AIAA 2019-1863

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

  9. 2018
  10. Published

    TOWARDS THE DEVELOPMENT OF BIOINSPIRED ROTORS FOR EFFICIENT MICRO AIR VEHICLES

    Rezgui, D. & Jung, B., 14 Nov 2018, International Powered Lift Conference.

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

  11. Published

    Nonlinear stability analysis of whirl flutter in a rotor-nacelle system

    Mair, C., Rezgui, D. & Titurus, B., Nov 2018, In : Nonlinear Dynamics. 94, 3, p. 2013-2032 20 p.

    Research output: Contribution to journalArticle

  12. Published

    Testing of a hinged wing-tip device for gust loads alleviation

    Cheung, R., Rezgui, D., Cooper, J. & Wilson, T., Sep 2018, In : Journal of Aircraft. 37 p.

    Research output: Contribution to journalArticle

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