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Showing 1 to 8 of 8 for “"Gulfstream"”.

  1. Gulfstream Aerospace Aircraft Static Position Utility

    … utility developed for commercial application by Gulfstream Aerospace employees and customers to determine static position data of Gulfstream aircraft. The static position data includes aircraft attitude, nose and main landing gear loads and aircraft ground clearance data.</p> <p>The previous …

    gsu Repository record for Gulfstream Aerospace Aircraft Static Position Utility (opens in a new tab)

  2. Development of Automatic CFD Grid Generation for the Design of the Preliminary Wing Sweep Schedule for the Gulfstream Quiet Supersonic Jet

    <p>The wing sweep schedule for the Gulfstream Quiet Supersonic Jet (wing and body) was investigated using CFD analysis methods. The use of automating the gridding procedure allowed for numerous cases to be investigated. The examination of the drag polar for different Mach cases indicated the …

    embry-riddle Repository record for Development of Automatic CFD Grid Generation for the Design of the Preliminary Wing Sweep Schedule for the Gulfstream Quiet Supersonic Jet (opens in a new tab)

  3. The Design for Manufacturing and Assembly Analysis and Redesign of an Aircraft Refueling Door Hinge Utilizing Additive Manufacturing

    … an aircraft door hinge assembly provided by Gulfstream Aerospace was analyzed following an established process called DFMA. The hinge was then redesigned to be additively manufactured, which is uncommon currently in industry for load bearing components. It was shown that the Design for …

    embry-riddle Repository record for The Design for Manufacturing and Assembly Analysis and Redesign of an Aircraft Refueling Door Hinge Utilizing Additive Manufacturing (opens in a new tab)

  4. Wind tunnel testing of a nacelle bypass concept for a quiet supersonic aircraft

    … flight conditions. One technology proposed by Gulfstream Aerospace Corporation for the production of low-noise supersonic aircraft is the high-flow nacelle bypass concept in which an outer nacelle surface is used to encircle the asymmetric external engine protuberances of a traditional turbine …

    uiuc Repository record for Wind tunnel testing of a nacelle bypass concept for a quiet supersonic aircraft (opens in a new tab)

  5. Heterogeneous (HG) Blankets for Improved Aircraft Interior Noise Reduction

    … A full-scale fuselage experiment performed on a Gulfstream section involves using the design tool for the positions of the mass inclusions, and the results of the previously described empirical approach facilitate tuning of the natural frequencies of the mass inclusions to the desired natural …

    vt Repository record for Heterogeneous (HG) Blankets for Improved Aircraft Interior Noise Reduction (opens in a new tab)

  6. Design and development of a rectangular supersonic wind tunnel facility for the study of shock/boundary layer interactions

    … supersonic inlet project conducted by NASA, Gulfstream Aerospace Corporation, Rolls-Royce, and the University of Illinois. The low-boom supersonic inlet project itself was part of a new supersonic business jet design. The primary goal of the low-boom supersonic inlet group was to reduce the …

    uiuc Repository record for Design and development of a rectangular supersonic wind tunnel facility for the study of shock/boundary layer interactions (opens in a new tab)

  7. Variability of water masses and circulation in the subtropical North Atlantic

    … minimum phase in the NAO, does not intensify the GulfStream in the manner of excess cooling. It is concluded that 18 Water is more strongly renewed, with accompanying Gulf Stream intensification, under NAO-minimum buoyancy forcing.

    soton Repository record for Variability of water masses and circulation in the subtropical North Atlantic (opens in a new tab)

  8. An experimental study of the aft guide vanes of an engine bypass nacelle for low-boom supersonic flight

    Due to the large disturbance created by the sonic boom, supersonic flight is strictly controlled by the FAA. One way in which to minimize the sonic boom is through shape-tailoring of the aircraft body and of the propulsion system. To this end, a new supersonic engine concept has been proposed, …

    uiuc Repository record for An experimental study of the aft guide vanes of an engine bypass nacelle for low-boom supersonic flight (opens in a new tab)