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Model tests of gliding with different hindwing configurations in the four-winged dromaeosaurid Microraptor gui

机译:四翼Dromaeosaurid Microraptor gui中具有不同后翼配置的滑翔模型测试

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摘要

Fossils of the remarkable dromaeosaurid Microraptor gui and relatives clearly show well-developed flight feathers on the hind limbs as well as the front limbs. No modern vertebrate has hind limbs functioning as independent, fully developed wings; so, lacking a living example, little agreement exists on the functional morphology or likely flight configuration of the hindwing. Using a detailed reconstruction based on the actual skeleton of one individual, cast in the round, we developed light-weight, three-dimensional physical models and performed glide tests with anatomically reasonable hindwing configurations. Models were tested with hindwings abducted and extended laterally, as well as with a previously described biplane configuration. Although the hip joint requires the hindwing to have at least 20° of negative dihedral (anhedral), all configurations were quite stable gliders. Glide angles ranged from 3° to 21° with a mean estimated equilibrium angle of 13.7°, giving a lift to drag ratio of 4.1:1 and a lift coefficient of 0.64. The abducted hindwing model's equilibrium glide speed corresponds to a glide speed in the living animal of 10.6 m·s~(-1). Although the biplane model glided almost as well as the other models, it was structurally deficient and required an unlikely weight distribution (very heavy head) for stable gliding. Our model with laterally abducted hindwings represents a biologically and aerodynamically reasonable configuration for this four-winged gliding animal. M. gui's feathered hindwings, although effective for gliding, would have seriously hampered terrestrial locomotion.
机译:杰出的蜥脚类蜥蜴的化石及其亲属的化石清楚地在后肢和前肢显示出发达的飞行羽毛。没有现代脊椎动物的后肢具有独立的,完全发达的翅膀的功能。因此,缺乏活生生的例子,在后翼的功能形态或可能的飞行形态方面几乎没有共识。使用基于一个人的真实骨骼的详细重建,并进行全面铸造,我们开发了重量轻的三维物理模型,并在解剖学上合理的后翼配置下进行了滑行测试。在绑架后肢并横向延伸的情况下,以及先前描述的双翼飞机配置,对模型进行了测试。尽管髋关节要求后尾至少有20°的负二面角(anhedral),但所有配置都是相当稳定的滑翔机。滑翔角范围为3°至21°,平均估计平衡角为13.7°,升力/阻力比为4.1:1,升力系数为0.64。被绑架的后掠模型的平衡滑行速度对应于活动物中的滑行速度为10.6 m·s〜(-1)。尽管双翼飞机模型的滑行几乎与其他模型一样,但它在结构上存在缺陷,并且需要不大的重量分布(非常重的头部)才能稳定滑行。我们的带有后绑架侧翼的模型代表了这种四翼滑翔动物的生物学和空气动力学合理配置。圭先生的羽毛后肢虽然可以滑行,但会严重阻碍地面运动。

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  • 作者单位

    Department of Ecology & Evolutionary Biology, University of Kansas, Lawrence, KS 66045-7534;

    rnDepartment of Geology, Northeastern University, Shenyang, Liaoning 110004, China;

    rnDepartment of Ecology & Evolutionary Biology, University of Kansas, Lawrence, KS 66045-7534 Division of Paleontology, Biodiversity Institute, University of Kansas, Lawrence, KS 66045-7561;

    rnDivision of Paleontology, Biodiversity Institute, University of Kansas, Lawrence, KS 66045-7561;

    rnDivision of Paleontology, Biodiversity Institute, University of Kansas, Lawrence, KS 66045-7561 Department of Geology, University of Kansas, Lawrence, KS 66045-7613;

  • 收录信息 美国《科学引文索引》(SCI);美国《生物学医学文摘》(MEDLINE);美国《化学文摘》(CA);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    biomechanics; bird flight evolution; feathered dinosaurs; model tests; tetrapteryx;

    机译:生物力学鸟类飞行进化;羽毛恐龙模型测试;四翼类;
  • 入库时间 2022-08-18 00:41:15

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