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- W2314076143 abstract "Most of procedures available in conceptual design estimate airframe weight by statistical methods and do not take into account for aeroelastic requirements, postponing them to successive more detailed design phases. If the former task is not based on sound structural principles, the estimation will be likely to be unreasonable and results in serious difficulties, especially when non-conventional layouts are considered. Indeed, a large error in weight estimation will usually have far-reaching effects in the whole project; such errors have sometimes been the main factors in the unsuccessful designs. Furthermore, the late discovery of adverse aeroelastic issues may result in significant re-design costs, considerable changes in the structural design, limitations in flight envelope, weight penalties, and in some cases, it may even require to actually close the project. Thus, in order to overcome the insurgence of these issues, the influence of deformability on flight and handling performances, on structural weight and on design costs needs to be taken into account as early as possible in the design process. NeoCASS (Next generation Conceptual Aero-Structural Sizing Suite) enables the creation of efficient low-order, medium fidelity models particularly suitable for structural sizing, aeroelastic analysis and optimization at the conceptual design level. It provides the total structural weight on physical basis, reducing to the minimum the adoption of statistics, and includes aeroelastic requirements and performances from the very beginning of the conceptual design phase. The whole methodology is based upon the integration of geometry construction, aerodynamic and structural analysis codes that combine depictive, computational, analytical, and semiempirical methods, validated in an aircraft design environment." @default.
- W2314076143 created "2016-06-24" @default.
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- W2314076143 date "2009-05-04" @default.
- W2314076143 modified "2023-09-25" @default.
- W2314076143 title "A Fast Tool for Structural Sizing, Aeroelastic Analysis and Optimization in Aircraft Conceptual Design" @default.
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- W2314076143 doi "https://doi.org/10.2514/6.2009-2571" @default.
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