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Showing 1 to 4 of 4 for “"Supersonic Aircraft Design"”.

  1. Verification and Validation of Open-Source Simulation Tools for Supersonic Aircraft Aerodynamic Analysis

    … for several flow problems relevant to the supersonic aerodynamics of small-scale, autonomous aircraft concepts. Vehicle concepts used as research platforms to test new aerospace technologies, such as advanced propulsion systems or large sensor payloads, require major modifications to …

    calgary Repository record for Verification and Validation of Open-Source Simulation Tools for Supersonic Aircraft Aerodynamic Analysis (opens in a new tab)

  2. Development of an Interactive Wave Drag Capability for the OpenVSP Parametric Geometry Tool

    … to successful and efficient transonic and supersonic flight. Area-ruling is the process of managing the cross-sectional area of an aircraft to lessen the wave drag experienced in flight. Effectively calculating the necessary areas for a given aircraft can be difficult, and existing tools …

    calpoly Repository record for Development of an Interactive Wave Drag Capability for the OpenVSP Parametric Geometry Tool (opens in a new tab)

  3. Constraining climate impact uncertainties from future aviation

    … technologies such as unmanned aerial vehicles, supersonic aviation, or hydrogen and alternative fuels. These factors together require a persistent effort to improve the available tools assessing aviation environmental footprint. The objective of this thesis is to provide additional insights into …

    mit Repository record for Constraining climate impact uncertainties from future aviation (opens in a new tab)

  4. Optimization of Supersonic Aircraft Wing-Box using Curvilinear SpaRibs

    … curvilinear spars and ribs, termed SpaRibs, to design supersonic aircraft wing-box in comparison to the use of classic design concepts that employ straight spars and ribs. The intent is to achieve a more efficient load-bearing mechanism and to passively control aeorelastic behavior of the …

    vt Repository record for Optimization of Supersonic Aircraft Wing-Box using Curvilinear SpaRibs (opens in a new tab)