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Showing 1 to 20 of 294 for “"trailing edge"”.

  1. Trailing Edge Aerodynamics: Flow Regimes, Geometry and Loss

    The flow at the trailing edge of a turbine blade at transonic air velocities can be extremely complex. Solid trailing edges can shed vortices in a manner known as transonic vortex shedding, where vortices form very close to the trailing edge and cause large trailing edge shear layer deflection. …

    cambridge Repository record for Trailing Edge Aerodynamics: Flow Regimes, Geometry and Loss (opens in a new tab)

  2. Helicopter rotor smoothing with a continuous trailing - edge flap

    … rotor smoothing process with a continuous trailing-edge flap (CTEF). The CTEF is a monolithic active blade control design with no mechanical linkages compared to the conventional discrete trailing-edge flap (DTEF). In this design, micro fiber composite (MFC) layers are embedded inside the …

    alabama Repository record for Helicopter rotor smoothing with a continuous trailing - edge flap (opens in a new tab)

  3. Investigation of high reduced frequency, separated trailing edge flows

    Thesis (Sc. D.)--Massachusetts Institute of Technology, Dept. of Ocean Engineering, 1996.

    mit Repository record for Investigation of high reduced frequency, separated trailing edge flows (opens in a new tab)

  4. Bio-Inspired Control of Roughness and Trailing Edge Noise

    … a separate new device for the reduction of trailing edge noise. This type of noise is generated by flow past the wing of an aircraft or the blades of a wind turbine, and is a source of annoyance for those in surrounding communities. The newly developed treatment consists of small fins, or …

    vt Repository record for Bio-Inspired Control of Roughness and Trailing Edge Noise (opens in a new tab)

  5. Trailing Edge Flow Conditions as a Factor in Airfoil Design

    … the role played by the non-dimensional trailing edge velocity in design is considered and the relationship between the specified value and the resulting airfoil geometry is explored. In addition, the ramifications of the unbounded trailing edge pressure gradients generally present in the …

    uiuc Repository record for Trailing Edge Flow Conditions as a Factor in Airfoil Design (opens in a new tab)

  6. Stator loading measurements behind a fan with trailing edge blowing

    The effects of trailing edge blowing on stator unsteady loading were investigated through a set of experiments on a trailing edge blowing fan. Flow field measurements and stator unsteady loading measurements were taken at five radial locations. Reductions in the relative wake harmonics were seen at …

    mit Repository record for Stator loading measurements behind a fan with trailing edge blowing (opens in a new tab)

  7. Turbofan rotor/stator interaction noise reduction through trailing edge blowing

    Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1998.

    mit Repository record for Turbofan rotor/stator interaction noise reduction through trailing edge blowing (opens in a new tab)

  8. Trailing-Edge Blowing of Model Fan Blades for Wake Management

    … to implement the wake management technique of trailing-edge blowing were tested in a linear cascade configuration. Measurements were made on two sets of blowing blades installed in the Virginia Tech low-speed linear cascade wind tunnel. The simple blowing blades were identical to the baseline …

    vt Repository record for Trailing-Edge Blowing of Model Fan Blades for Wake Management (opens in a new tab)

  9. Reduction of Unsteady Rotor-Stator Interaction Using Trailing Edge Blowing

    … to assess the effects of adding mass flow at the trailing edges of four stators upstream of an aircraft engine simulator. By using trailing edge blowing to minimize the shed wakes of the stators, the flow into the rotor was made more uniform. In these experiments a reduced number of stators (four) …

    vt Repository record for Reduction of Unsteady Rotor-Stator Interaction Using Trailing Edge Blowing (opens in a new tab)

  10. Prediction of Trailing Edge Noise from Two-Point Velocity Correlations

    … developed by Glegg et al. (2004) for solving the trailing edge noise problem. This method is based on the premises that the noise produced by a surface can be computed by the integral of the cross product between the velocity and vorticity fields, of the boundary layer and shed vorticity (Howe …

    vt Repository record for Prediction of Trailing Edge Noise from Two-Point Velocity Correlations (opens in a new tab)

  11. Bio-Inspired Trailing Edge Noise Control: Acoustic and Flow Measurements

    Trailing edge noise control is an important problem associated mainly with wind turbines. As turbulence in the air flows over a wind turbine blade, it impacts the trailing edge and scatters, producing noise. Traditional methods of noise control involve modifying the physical trailing edge, or the …

    vt Repository record for Bio-Inspired Trailing Edge Noise Control: Acoustic and Flow Measurements (opens in a new tab)

  12. Unsteady airfoil pressures induced by perturbation of the trailing edge flow

    Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1981.

    mit Repository record for Unsteady airfoil pressures induced by perturbation of the trailing edge flow (opens in a new tab)

  13. Advanced Trailing Edge Blowing Concepts for Fan Noise Control: Experimental Validation

    This thesis documents trailing edge blowing research performed to reduce rotor / stator interaction noise in turbofan engines. The existing technique of filling every velocity deficit requires a large amount of air and is therefore impractical. The purpose of this research is to investigate new …

    vt Repository record for Advanced Trailing Edge Blowing Concepts for Fan Noise Control: Experimental Validation (opens in a new tab)

  14. Numerical Study of Synthetic-Jet Actuation Effect on Airfoil Trailing Edge Noise

    <p>The current study conducts numerical simulations to assess the possibility of employing Synthetic Jet Actuators (SJAs) as active noise control devices for reduction of airfoil acoustic radiation. High-accuracy numerical efforts employ a sixth-order accurate Navier-Strokes solver implementing a …

    embry-riddle Repository record for Numerical Study of Synthetic-Jet Actuation Effect on Airfoil Trailing Edge Noise (opens in a new tab)

  15. Noise Reduction in an Axisymmetric Supersonic Aircraft Inlet using Trailing Edge Blowing

    … of a supersonic aircraft engine inlet using Trailing Edge Blowing (TEB) to reduce the engine fan noise from a turbofan propulsion simulator (TPS). The TPS is 4.1 in. (10.4 cm) in diameter and is powered by compressed air. The supersonic inlet is connected to the TPS and is geometrically and …

    vt Repository record for Noise Reduction in an Axisymmetric Supersonic Aircraft Inlet using Trailing Edge Blowing (opens in a new tab)

  16. Generation of Downstream Vorticity Through the Use of Modified Trailing Edge Configurations

    … were taken downstream of several modified trailing edge configurations designed to impart streamwise velocity into the flow behind a cascade of GE Rotor B fan blades. These measurements were conducted in the Virginia Tech Low Speed Linear Cascade wind tunnel. The trailing edge

    vt Repository record for Generation of Downstream Vorticity Through the Use of Modified Trailing Edge Configurations (opens in a new tab)

  17. The Influence of Trailing Edge Shape and Kinematics on Bio-inspired Pitching Panels

    … cases of rigid rectangular panels with varying trailing edge shape oscillating in pure pitch.</p> <p>In the current work, bio-inspired propulsion is examined through an investigation of multiple rigid pitching panels of trapezoidal planforms with trailing edge shapes that were varied in a …

    syracuse-diss Repository record for The Influence of Trailing Edge Shape and Kinematics on Bio-inspired Pitching Panels (opens in a new tab)

  18. Understanding the Impact of a Serrated Trailing Edge on the Unsteady Hydrodynamic Field

    Trailing edge noise is a common noise source in aerodynamic applications, such as wind turbines, duct fan blades, and propellers. As sound is a nuisance for people near this machinery, methods of reducing trailing edge noise are being investigated. A proven method of trailing edge noise reduction …

    vt Repository record for Understanding the Impact of a Serrated Trailing Edge on the Unsteady Hydrodynamic Field (opens in a new tab)

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