Fuel burn evaluation of a transonic strut-braced-wing regional aircraft through multipoint aerodynamic optimisation
نویسندگان
چکیده
Abstract This paper presents a relative fuel burn evaluation of the transonic strut-braced-wing configuration for regional aircraft class in comparison to an equivalent conventional tube-and-wing aircraft. is accomplished through multipoint aerodynamic shape optimisation based on Reynolds-averaged Navier-Stokes equations. Aircraft concepts are first developed low-order multidisciplinary design missions and top-level requirements Embraer E190-E2. High-fidelity then applied wing–body–tail models each aircraft, with objective minimising weighted-average cruise drag over five-point operating envelope that includes nominal point, points at $\pm 10\%$ $C_L$ Mach 0.78, two high-speed 0.81. Design variables include angle-of-attack, wing (and strut) twist section degrees freedom, horizontal tail incidence, while nonlinear constraints constant lift, zero pitching moment, minimum strut volume, maximum thickness-to-chord ratios. Results show optimised strut-braced maintains similar features those single-point optimum, compromises on-design performance by only counts achieve up 11.6% reductions off-design conditions. Introducing estimates approximating full performance, results indicate jet offers 13.1% improvement lift-to-drag ratio 7.8% reduction block 500nmi mission when compared similarly E190-E2-like
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ژورنال
عنوان ژورنال: Journal of the Royal Aeronautical Society
سال: 2022
ISSN: ['2059-6464', '0001-9240']
DOI: https://doi.org/10.1017/aer.2022.64