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Showing 1 to 4 of 4 for “"Engine Nacelle"”.

  1. Interference Drag Due to Engine Nacelle Location for a Single-Aisle, Transonic Aircraft

    … surrogate model of the interference drag between nacelles and wing-fuselage systems suitable for the inclusion in a multidisciplinary design optimization (MDO) framework. The target aircraft was a single-aisle, transonic aircraft with a freestream Mach number of 0.8 at 35,000 feet and a design …

    vt Repository record for Interference Drag Due to Engine Nacelle Location for a Single-Aisle, Transonic Aircraft (opens in a new tab)

  2. Trim, Control, and Performance Effects in Variable-Complexity High-Speed Civil Transport Design

    … and thickness distribution, fuselage shape, engine placement and thrust, using 29 design variables. While adding trim and control it was found necessary to simultaneously consider landing gear integration. We include the engine-out and crosswind landing requirements, as well as engine nacelle

    vt Repository record for Trim, Control, and Performance Effects in Variable-Complexity High-Speed Civil Transport Design (opens in a new tab)

  3. Determining appropriate levels of robotic automation in commercial aircraft nacelle assembly

    … industrial robotics in the assembly of the engine nacelle inlet for a commercial aircraft. In addition to addressing the achievable level of automation, this thesis also reviews the evaluation of robotics vendor proposals and the accompanying financial justification requisite for …

    mit Repository record for Determining appropriate levels of robotic automation in commercial aircraft nacelle assembly (opens in a new tab)

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

    Made available in DSpace on 2011-08-25T22:16:42Z (GMT). No. of bitstreams: 3 Herrera_Arthur.pdf: 9040481 bytes, checksum: b1cb32088f9dbae91d7f22098b17feb2 (MD5) license.txt: 4064 bytes, checksum: e734bd04ed7c751742bd7380d9b55410 (MD5) Herrera_Arthur.docx: 22589106 bytes, checksum: …

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