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Showing 1 to 9 of 9 for “"Aerodynamic load."”.

  1. Actuator-Work Concepts Applied to Morphing and Conventional Aerodynamic Control Devices

    … parameter for the comparison of various aerodynamic control device configurations. This estimated "actuator work," or practical work as it will be referred to as in this thesis, is based on the aerodynamic and structural resistance to a control surface deflection. It is meant to represent …

    vt Repository record for Actuator-Work Concepts Applied to Morphing and Conventional Aerodynamic Control Devices (opens in a new tab)

  2. A Low-Cost Method of Airspeed Data Acquisition via Image Processing and Experimental Aerodymanic Load Calculation Using Panel Methods

    … primary structures that exhibit a time-dependent load memory. A project was undertaken to develop a service-life prediction method to better understand composite use in this market segment. Most general-aviation aircraft do not possess flight data acquisition systems to gather in-service …

    carleton Repository record for A Low-Cost Method of Airspeed Data Acquisition via Image Processing and Experimental Aerodymanic Load Calculation Using Panel Methods (opens in a new tab)

  3. A vortex-lattice method for Delta wing aerodynamics

    … edge separation. Numerical predictions for the aerodynamic loads and pressure distributions are compared with experimental data. A 75° Delta wing and a 60° Delta wing with Leading Edge Vortex flaps in uniform, symmetric and steady flow are studied. Uniform and cosine distributions are used to …

    vt Repository record for A vortex-lattice method for Delta wing aerodynamics (opens in a new tab)

  4. A numerical model of unsteady, subsonic aeroelastic behavior

    … has been developed. The technique accounts for aerodynamic nonlinearities associated with angles of attack, vortex-dominated flow, static deformations, and unsteady behavior. The angle of attack is limited only by the occurrence of stall or vortex bursting near the wing. The fluid and the wing …

    vt Repository record for A numerical model of unsteady, subsonic aeroelastic behavior (opens in a new tab)

  5. Structural analysis and multidisciplinary design of flexible fluid loaded composite canard

    … of a composite canard subject to static aerodynamic loads was numerically studied in the present research. The canard was modeled as a symmetrically laminated curved panel, consisting of 8 plies of T300/5208 graphite/epoxy composite laminate. Modeling of this structure-fluid interaction …

    iastate Repository record for Structural analysis and multidisciplinary design of flexible fluid loaded composite canard (opens in a new tab)

  6. Identification of Transient Nonlinear Aeroelastic Phenomena

    … aeroelastic phenomena include unsteady nonlinear aerodynamic loads, structural nonlinearities, as well as nonlinear couplings between the flow and the structural response. Nonlinearities in aerodynamic loads originate from unsteady shocks and/or flow separation. Structural nonlinearities are …

    vt Repository record for Identification of Transient Nonlinear Aeroelastic Phenomena (opens in a new tab)

  7. Helicopter Flight Dynamics Simulation with a Time-Accurate Free-Vortex Wake Model

    … dynamics were also studied and related to the aerodynamic load distributions obtained with the free wake induced velocities. The model was also validated in a lateral maneuver from hover. The results show improvements in the on-axis prediction, and indicate a possible relation between the …

    maryland Repository record for Helicopter Flight Dynamics Simulation with a Time-Accurate Free-Vortex Wake Model (opens in a new tab)

  8. Unsteady Aerodynamic and Aeroelastic Analysis of Flapping Flight

    The unsteady aerodynamic and aeroelastic analysis of flapping flight under various kinematics and flow parameters is presented in this dissertation. The main motivation for this study arises from the challenges facing the development of micro air vehicles. Micro air vehicles by requirement are …

    vt Repository record for Unsteady Aerodynamic and Aeroelastic Analysis of Flapping Flight (opens in a new tab)

  9. Agile load transportation systems using aerial robots

    … we address problems that can occur during load transport using aerial robots, i.e., small scale quadrotors. First, detailed models of such transportation system are derived. These models include nonlinear models of a quadrotor, a model of a quadrotor carrying a fixed load and a model of a …

    unm Repository record for Agile load transportation systems using aerial robots (opens in a new tab)