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Showing 1 to 10 of 10 for “"Morphing Aircraft"”.

  1. Feasibility of morphing aircraft propeller blades

    wichita-thes

  2. Control system design for morphing aircraft

    wichita-thes

  3. Dynamics and Control of Morphing Aircraft

    … work is directed towards an evaluation of aircraft that undergo structural shape change for the purpose of optimized flight and maneuvering control authority. Dynamical equations are derived for a morphing aircraft based on two primary representations; a general non-rigid model and a …

    vt Repository record for Dynamics and Control of Morphing Aircraft (opens in a new tab)

  4. Design, Development, and Analysis of a Morphing Aircraft Model for Wind Tunnel Experimentation

    Morphing aircraft combine both radical and subtle wing shape changes to improve vehicle performance relative to a rigid airframe. An aircraft wind tunnel model with considerable wing-shape freedom can serve as a tool in learning to model, control, and fully exploit the potential of such vehicles. …

    vt Repository record for Design, Development, and Analysis of a Morphing Aircraft Model for Wind Tunnel Experimentation (opens in a new tab)

  5. Investigation of Polymer-Filled Honeycomb Composites with Applications as Variable Stiffness Morphing Aircraft Structures

    Shape morphing in aerospace structures has the potential to reduce noise, improve efficiency, and increase the adaptability of aircraft. Among the many challenges in developing morphing technologies is finding suitable wing skin materials that can be both stiff to support the structural loads, …

    vt Repository record for Investigation of Polymer-Filled Honeycomb Composites with Applications as Variable Stiffness Morphing Aircraft Structures (opens in a new tab)

  6. Design Demonstration and Optimization of a Morphing Aircraft Control Surface Using Flexible Matrix Composite Actuators

    The morphing of aircraft wings for flight control started as a necessity for the Wright Brothers but quickly fell out of favor as aircraft increased speed. Currently morphing aircraft control is one of many ideas being explored as we seek to improve aircraft efficiency, reduce noise, and other …

    vt Repository record for Design Demonstration and Optimization of a Morphing Aircraft Control Surface Using Flexible Matrix Composite Actuators (opens in a new tab)

  7. Strain-based Topology Optimization of a 2D Morphing Transitional Surface

    Morphing aircraft offer many benefits. However, the design of stiff yet flexible structures still provides many obstacles to fully exploring and realizing morphing structures. Due to this, many morphing challenges remain open. Topology optimization is a type of structural optimization that …

    vt Repository record for Strain-based Topology Optimization of a 2D Morphing Transitional Surface (opens in a new tab)

  8. Nonlinear Controller Design for UAVs with Time-Varying Aerodynamic Uncertainties

    … era of more powerful and versatile UAVs (e.g. morphing aircraft), able to perform a variety of missions. This dissertation presents a novel, comprehensive, step-by-step, nonlinear controller design framework for new generation, non-conventional UAVs with time-varying aerodynamic characteristics …

    denver Repository record for Nonlinear Controller Design for UAVs with Time-Varying Aerodynamic Uncertainties (opens in a new tab)

  9. Supermanoeuvrability in a biomimetic morphing-wing aircraft

    … study the supermanoeuvrability of a biomimetic morphing-wing case study aircraft system. Analytical and computational models of biomimetic flight dynamics are developed, utilising multibody dynamics, computational fluid dynamics, and reduced-order aerodynamic models; and validated with respect …

    cambridge Repository record for Supermanoeuvrability in a biomimetic morphing-wing aircraft (opens in a new tab)

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

    … surface cases, it is found that a quadratic (morphing) trailing edge flap requires less practical work than a linear flap of the same size. As the angle of attack at which the change in lift occurs increases, the benefit of the quadratic flap becomes greater. For multiple control surface …

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