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Showing 1 to 9 of 9 for “"helicopter rotor blade"”.

  1. Characterization of active fiber composite actuators for helicopter rotor blade applications

    Wickramasinghe, Viresh K. (Viresh Kanchana), 1971-Massachusetts Institute of Technology2001

    Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2001.

    mit Repository record

  2. Modelling and stability analysis of a composite helicopter rotor blade with integrated active fibres

    Saxton, Caroline R.Carleton University2003

    carleton Repository record

  3. Helicopter rotor blade loading calculations using an axisymmetric vortex sheet and the free wake method

    Huh, Kevin S. (Kevin Sangmin)Massachusetts Institute of Technology1988

    Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1988.

    mit Repository record

  4. On the indentification of harmonic loads and inflow of a coupled bending-torsion helicopter rotor blade

    Higman, Jerry PaulGeorgia Institute of Technology1996

    gatech Repository record

  5. Application of the Filtered-X LMS Algorithm for Disturbance Rejection in Time-Periodic Systems

    Fowler, Leslie PaigeVirginia Tech1996

    … generalized linear, time-periodic system and the helicopter rotor blade in forward flight. Results for the generalized system show that the filtered-X LMS algorithm does converge for time-periodic disturbance inputs and can produce very small errors. For the helicopter rotor blade system the …

    vt Repository record

  6. Rotor Blade Flap-Lag Stability and Response in Forward Flight in Turbulent Flows

    Shiau, Ting-Nung BernardUniversity of Illinois at Urbana-Champaign2014

    … turbulence on the coupled flap-lag motion of a helicopter rotor blade in forward flight is investigated. By assuming white noise turbulence and applying a special case of the stochastic averaging procedure, equations are developed which describe the stochastic first and second moments of the …

    uiuc Repository record

  7. A Combined Piezoelectric Composite Actuator and Its Application to Wing/Blade Tips

    Ha, KwangtaeGeorgia Institute of Technology2005

    … as a hinge tension-torsion bar actuator for a helicopter rotor blade flap or blade tip and mirror rotational positioning. In the wing tip case, the tip deflection angle is different only according to the aerodynamic moment depending on the hinge position of the actuator along the chord and …

    gatech Repository record

  8. Dynamical System Representation and Analysis of Unsteady Flow and Fluid-Structure Interactions

    Hussein, Ahmed Abd Elmonem AhmedVirginia Tech2018

    … second chapter, I investigate the flutter of a helicopter rotor blade using finite-state time approximation of the unsteady aerodynamics. The analysis showed a new stability region that could not be determined under the assumption of a quasi-steady flow. In the third chapter, I implement the …

    vt Repository record

  9. Numerical Simulations and Studies on Round Jet Impingement, Twin Jet Impingement and Helicopter Rotor Blades Ground Effect

    Gao, Han2018

    … effect. The third part focuses on a 3-D helicopter rotor blade with ground effect. The result firstly demonstrated that modern technology has ability to make a well-matched CFD result. Then it explored changing pattern of the flow field with different angles of attack and non-dimensional …

    wustl Repository record