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Showing 1 to 3 of 3 for “"inboard wing"”.

  1. Aerodynamic Properties of the Inboard Wing Concept

    … the fuselages at the tips of a low aspect ratio wing. The motivation for this configuration is to provide an increase in the number of passengers carried with no increase in span over conventional designs. An additional motivation is the change in the wake flow of the wing, due to the fuselages …

    vt Repository record for Aerodynamic Properties of the Inboard Wing Concept (opens in a new tab)

  2. Time-Domain Simulations of Aerodynamic Forces on Three-Dimensional Configurations, Unstable Aeroelastic Responses, and Control by Neural Network Systems

    … interactions between aerodynamic forces and wing structures are numerically investigated as integrated dynamic systems, including structural models, aerodynamics, and control systems, in the time domain. An elastic beam model coupled with rigid-body rotation is developed for the wing

    vt Repository record for Time-Domain Simulations of Aerodynamic Forces on Three-Dimensional Configurations, Unstable Aeroelastic Responses, and Control by Neural Network Systems (opens in a new tab)

  3. A Self-Sustaining, Boundary-Layer-Adapted System for Terrain Exploration and Environmental Sampling

    This thesis describes the preliminary design of a system for remote terrain exploration and environmental sampling on worlds with dense atmospheres. The motivation for the system is to provide a platform for long-term scientific studies of these celestial bodies. The proposed system consists of …

    vt Repository record for A Self-Sustaining, Boundary-Layer-Adapted System for Terrain Exploration and Environmental Sampling (opens in a new tab)