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Simplified Aerodynamic and Structural Modeling for Oblique All-Wing Aircraft. Phase 2: Structures

机译：倾斜全翼飞机的简化空气动力学和结构模型。第2阶段：结构

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Any aircraft preliminary design study requires a structural model of the proposed configuration. The model must be capable of estimating the structural weight of a given configuration, and of predicting the deflections which will result from foreseen flight and ground loads. The present work develops such a model for the proposed Oblique All Wing airplane. The model is based on preliminary structural work done by Jack Williams and Peter Rudolph at Mdng, and is encoded in a FORTRAN program. As a stand-alone application, the program can calculate the weight CG location, and several types of structural deflections; used in conjunction with an aerodynamics model, the program can be used for mission analysis or sizing studies.

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作者
Kroo, I.;
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年度 1994
页码 1-19
总页数 19
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Oblique wings; Tailless aircraft; Predictions; Aircraft design; Aircraft models; Structural weight; Fortran; Applications programs(Computers); Aerodynamic loads; Aeronautical engineering; Center of gravity;

机译：斜翼;无尾飞机;预测;飞机设计;飞机模型;结构重量; Fortran;应用程序（计算机）;气动载荷;航空工程;重心;

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2. Simplified Modelling Of Joints And Beam-like Structures For Biw Optimization In A Concept Phase Of The Vehicle Design Process [J] . D. Mundo, R.Hadjit, S. Donders, Finite Elements in Analysis and Design . 2009,第6a7期

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3. Fluid-structure interaction analysis of NREL phase VI wind turbine: Aerodynamic force evaluation and structural analysis using FSI analysis [J] . Lee Kyoungsoo, Huque Ziaul, Kommalapati Raghava, Renewable energy . 2017,第deca期

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4. Oblique all-wing airliner sizing and cabin integration [C] . Rawdon Blaine K. SAE Conference . 1998

机译：倾斜全翼客机尺寸和机舱集成
5. Integrated aerodynamic and control system design of oblique wing aircraft. [D] . Morris, Stephen James. 1990

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6. Influence of Asymmetric Stiffness on the Structural and Aerodynamic Response of Synthetic Vocal Fold Models [O] . B.A. Pickup, S.L. Thomson -1

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7. Mechanism of aerodynamic force generation concerning train vibration in tunnel (LES of large-scale flow structure around simplified train model) [O] . Koji NAKADE, Yutaka SAKUMA, Takeo KAJISHIMA 2021

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8. Simplified Aerodynamic and Structural Modeling for Oblique All-Wing Aircraft. Phase 2: Structures [R] . 1994

机译：倾斜全翼飞机的简化空气动力学和结构模型。阶段2：结构

Simplified Aerodynamic and Structural Modeling for Oblique All-Wing Aircraft. Phase 2: Structures

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