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- W2331036282 abstract "The center section of a hybrid wing body (HWB) transport aircraft must perform the dual role of containing the pressurized passenger cabin and providing a significant percentage of vehicle lift. Since a vehicle of this type has never been in production, empirical models and historical data for conceptual phase sizing and performance evaluations do not exist. Therefore, early structural sizing for the HWB has shifted toward computational physics-based modeling to obtain initial weight estimates. These integrated computational environments implement assumptions consistent with the early phases of design, but may not capture important aero-structural interactions of the HWB centerbody. This paper introduces one of the potential interactions and behavior is characterized for varying levels of assumptions and models. PRSEUS was applied to the upper and lower surface of the NASA/Boeing N2A HWB centerbody, using conceptual level “smeared” skin properties and higher level discretely modeled stiffeners. Deflections were recorded under internal pressure loads and the effect of the deflections on centerline 2-D aerodynamics is shown for potential flow and inviscid compressible flow." @default.
- W2331036282 created "2016-06-24" @default.
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- W2331036282 date "2014-06-13" @default.
- W2331036282 modified "2023-09-23" @default.
- W2331036282 title "Characterization of an Aero-Structural Interaction for the Hybrid Wing Body Center Section in Conceptual Phase Structural Sizing" @default.
- W2331036282 cites W2021364443 @default.
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- W2331036282 doi "https://doi.org/10.2514/6.2014-3159" @default.
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