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- W2321848895 abstract "The design of advanced aircraft that simultaneously meet increasingly strict noise, emissions, and fuel burn requirements will require accurate analysis of propulsion-airframe integration effects even at the conceptual design level. To meet this requirement, there is a need for new, easy-to-use parametric-based geometry and modeling analysis methodologies. This paper presents a research strategy to develop improved parametric geometry tools suitable for incorporation into an automated or batch-mode Multidisciplinary Design, Analysis and Optimization (MDAO) environment., and to develop an improved capability for 3D representation of the engine internal flowpath, in order to permit more detailed analyses of the engine cycle selection for highly integrated vehicle concepts. The primary tools utilized in this research include the NASA-developed programs Numerical Propulsion System Simulation (NPSS), Weight Analysis for Turbine Engines (WATE++), and Vehicle Sketch Pad (VSP)." @default.
- W2321848895 created "2016-06-24" @default.
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- W2321848895 date "2012-01-09" @default.
- W2321848895 modified "2023-09-26" @default.
- W2321848895 title "Parametric Geometry for Propulsion-Airframe Integration" @default.
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- W2321848895 doi "https://doi.org/10.2514/6.2012-548" @default.
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