Global ETD Search

Search theses and dissertations gathered from participating repositories worldwide. Every result links back to the library that holds it. No account is needed.

Results

Showing 1 to 11 of 11 for “"Aircraft Icing"”.

  1. Inflight Characterization of Aircraft Icing

    … as an additional layer of safety against aircraft icing accidents, by presenting and validating a conceptual design for the icing characterization function of the IMS. This icing characterization function seeks to provide a near real-time estimate of the degradation of the aircraft flight …

    uiuc Repository record for Inflight Characterization of Aircraft Icing (opens in a new tab)

  2. A machine learning study of wind-driven runback/flow-off multiphase flows pertinent to aircraft icing phenomena

    In-flight icing and ground icing are widely recognized hazards that have a substantial impact on the safety of aircraft during the processes of takeoff, cruising, and landing in cold weather conditions. The unsteady runback behavior of wind-driven runback water film (WDRWF) flows over aircraft

    iastate Repository record for A machine learning study of wind-driven runback/flow-off multiphase flows pertinent to aircraft icing phenomena (opens in a new tab)

  3. Numerical study of linearized unsteady stagnation flow

    … flows for application to problems involving aircraft icing. In this study, numerical methods which can be used to address the stability and non-parallel unsteady development of such stagnation point problems are investigated for linearized single phase aerodynamic flows using both …

    iastate Repository record for Numerical study of linearized unsteady stagnation flow (opens in a new tab)

  4. Impact Dynamics of Water Droplet on Solid Surfaces: Effect of Impact Reynolds Number, Hydrophobicity, Surface Roughness and Temperature

    … and aviation industries are dealing with is aircraft icing. The impact and freezing process of a water droplet on a cold surface has been investigated over time in order to develop preventative methods for avoiding icing. In the present study, we examined the behavior of a water droplet …

    vt Repository record for Impact Dynamics of Water Droplet on Solid Surfaces: Effect of Impact Reynolds Number, Hydrophobicity, Surface Roughness and Temperature (opens in a new tab)

  5. Finite Element Modeling of Macro Fiber Composite Actuators with Application to Wing De-icing

    <p>Icing can have a profound impact on aircraft performance during inclement weather conditions. Aircraft icing primarily occurs on the leading edge of wings, tails and engines. The de-icing/anti-icing technologies currently in use are typically bulky, heavy, cover the entire airfoil surface and …

    embry-riddle Repository record for Finite Element Modeling of Macro Fiber Composite Actuators with Application to Wing De-icing (opens in a new tab)

  6. Validation of 3-D ice accretion documentation and replication method including pressure-sensitive paint

    … is important to the study and understanding of aircraft icing. For research and certification purposes, replicas of ice accretions generated from icing wind tunnels are fabricated to perform aerodynamic tests in dry-air wind tunnels. The currently employed replication method consists of creating …

    uiuc Repository record for Validation of 3-D ice accretion documentation and replication method including pressure-sensitive paint (opens in a new tab)

  7. Lagrangian Parcel Volume method applied to icing surfaces to predict impact efficiency

    … to predict how and where ice will accrete on an aircraft, engineers first need to be able to track the path and concentration of water particles; this will allow for a better representation of water impingement and ice accretion. This tracking can be accomplished by using either a Lagrangian …

    uiuc Repository record for Lagrangian Parcel Volume method applied to icing surfaces to predict impact efficiency (opens in a new tab)

  8. Aerodynamics of a swept wing with leading-edge ice at low Reynolds number

    An experimental study of the aerodynamics of a swept wing with ice at low Reynolds number has been performed. The goal of this work was to demonstrate the use of various experimental techniques applied to understanding the aerodynamic effects of a leading-edge ice simulation on a highly swept, …

    uiuc Repository record for Aerodynamics of a swept wing with leading-edge ice at low Reynolds number (opens in a new tab)

  9. Computational Modeling of Droplet Impact Dynamics on Solid Substrates

    … flow environment. Focusing on research from an aircraft de-icing point of view, this study is considered a prerequisite in understanding the physics of droplet impact. The primary focus is on extending the application to incorporate super-cooled environments. Development of the model involved …

    vt Repository record for Computational Modeling of Droplet Impact Dynamics on Solid Substrates (opens in a new tab)

  10. Design of 3D swept wing hybrid models for icing wind tunnel tests

    The study of aircraft icing is critical to ensure the safety of any aircraft that might experience icing conditions in flight, including general, commercial, and military aviation. The certification of modern commercial transports requires manufacturers to demonstrate that these aircraft can safely …

    uiuc Repository record for Design of 3D swept wing hybrid models for icing wind tunnel tests (opens in a new tab)

  11. Large-scale swept-wing ice accretion modeling in the NASA Glenn Icing Research Tunnel using LEWICE3D

    The study of aircraft icing is necessary to ensure the safety of commercial, military, and general aviation aircraft. The certification of modern commercial transports requires manufacturers to demonstrate that these aircraft can safely operate during icing conditions consistent with the standards …

    uiuc Repository record for Large-scale swept-wing ice accretion modeling in the NASA Glenn Icing Research Tunnel using LEWICE3D (opens in a new tab)