Global ETD Search

Search theses and dissertations gathered from participating repositories worldwide. Every result links back to the library that holds it. No account is needed.

Results

Showing 1 to 3 of 3 for “"Tip-Mounted Engines"”.

  1. Structural Optimization and Design of a Strut-Braced Wing Aircraft

    … aspect ratio wing with thin airfoil sections and tip-mounted engines. However, such wing structures could suffer from a significant weight penalty. Thus, the use of an external strut or a truss bracing is promising for weight reduction. Due to the unconventional nature of the proposed concept, …

    vt Repository record for Structural Optimization and Design of a Strut-Braced Wing Aircraft (opens in a new tab)

  2. Multidisciplinary Design Optimization of a Strut-Braced Wing Aircraft

    … to achieve natural laminar flow. Additionally, tip-mounted engines can be used to reduce the induced drag. The MDO approach helps the designer achieve the best technology integration by making optimum trades between competing physical effects in the design space. To perform this study, a suite …

    vt Repository record for Multidisciplinary Design Optimization of a Strut-Braced Wing Aircraft (opens in a new tab)

  3. The Role of Constraints and Vehicle Concepts in Transport Design: A Comparison of Cantilever and Strut-Braced Wing Airplane Concepts

    … are examined: cantilever wing aircraft, fuselage mounted engine SBW, wing mounted engine SBW, and wingtip mounted engine SBW. The cantilever wing design is used as a baseline for comparison. Two mission profiles were used. The first called for a 7380 nmi range with a 305 passenger load based on a …

    vt Repository record for The Role of Constraints and Vehicle Concepts in Transport Design: A Comparison of Cantilever and Strut-Braced Wing Airplane Concepts (opens in a new tab)