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CAREER: Investigation of Dynamic Interactions Between Wing-Body and Aerodynamics in Bio-Inspired Flight

CAREER: Investigation of Dynamic Interactions Between Wing-Body and Aerodynamics in Bio-Inspired Flight
职业:研究仿生飞行中翼身与空气动力学之间的动态相互作用
批准号:
1846308
负责人:
Haithem Taha
金额:
$50.0万
依托单位国家:
美国
项目类别:
Standard Grant
财政年份:
2019
资助国家:
美国
项目状态:
已结题
起止时间:
2019-03-15 至 2024-02-29

项目摘要

项目成果

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中文摘要
翻译
昆虫和鸟类等生物飞行器在其自然机动能力方面代表了工程奇迹。这些展示的生物现象为解决问题提供了一个科学上丰富的金矿。这些飞行器所表现出的令人震惊的机动性能是它们扑动的翅膀和流过它们身体的流体产生的空气动力学之间发生的复杂动态相互作用的结果。 已经观察到一些昆虫执行大于3000度/秒的转向动作,延迟小于30毫秒。在正常的日常飞行中,一些鸟类在超重力任务中可能会经历高达14 g的加速度,而最先进的战斗机的机动性不能超过8-9 g。该教师早期职业发展计划(CAREER)项目将侧重于了解飞行过程中翼身和流体动力学之间动态相互作用的基本方面和机制。拟议研究的结果将使工程师能够通过促进自我(自然)稳定来设计生物启发的微型飞行器,而无需复杂的传感器控制执行器处理系统。这项研究将提高微型飞行器和无人机的设计能力,这些飞行器和无人机在搜索和救援任务、侦察任务、拍摄、边境监测、应急响应等方面具有巨大的潜在用途。这是一项多学科的工作,弥合了数学、物理、工程和生物力学之间的差距。该项目还将为学生开发新课程和有趣的计划,重点是提高少数民族学生在STEM学科的参与。 该建议的主要目的是研究扑翼飞行中翼身动力学和非定常流动力学之间的相互作用,特别强调新发现的振动稳定现象的基础物理。这将通过一种三管齐下的方法来实现:(i)理论:通过发展一种降阶飞行动力学模型,并利用几何控制理论和高阶平均来分析气动力-机身-机翼-动力学相互作用;(ii)计算:通过求解昆虫翅膀周围的纳维尔-斯托克斯方程,结合控制机翼和机身运动的力学方程,研究前缘和后缘涡在振动稳定现象中的作用;(iii)实验:通过建立一个多自由度的试验台(运动捕捉和流动可视化),以验证理论和计算结果,并通过实验评估振动稳定的扑翼飞行的有效性,并仔细检查其物理。最后,新一代的扑翼微型飞行器将依靠所发现的振动稳定现象,以最小的驱动力进行开发。该奖项反映了NSF的法定使命,并通过使用基金会的知识价值和更广泛的影响审查标准进行评估,被认为值得支持。
英文摘要
Biological flyers such as insects and birds represent an engineering marvel in terms of their natural maneuvering capabilities. These exhibited biological phenomena offer a scientifically-rich gold mine for problems. The astounding maneuvering performance exhibited by these flyers is a result of complex dynamic interaction that takes place between their flapping wings and the aerodynamics resulting from fluid flow over their bodies. Some insects have been observed to perform turning maneuvers of greater than 3000 deg/s, with less than a 30 ms delay. In normal everyday flight, some birds may experience up to 14 g accelerations in super-maneuverable tasks, while the maneuverability of the most advanced fighter airplanes cannot exceed 8-9 g. This Faculty Early Career Development Program (CAREER) project will focus on understanding the fundamental aspects and mechanisms of the dynamic interaction between the wing-body and fluid dynamics during flight. The results from the proposed research will enable engineers to design bio-inspired micro-air-vehicles without complicated sensory-control-actuator-processing systems by promoting self (natural) stabilization. The proposed research will boost the design capabilities of micro-air-vehicles and drones, which have great potential use in search and rescue missions, reconnaissance missions, filming, border monitoring, emergency response, etc. It is a multi-disciplinary work that bridges the gap between mathematics, physics, engineering, and biomechanics. The project will also lead to the development of new courses for students and interesting program that focuses on improving participation of minority students in STEM disciplines. The primary objective of this proposal is to investigate the interactions between the wing-body dynamics and unsteady flow dynamics in flapping flight with particular emphasis on the underpinning physics of the newly discovered vibrational stabilization phenomenon. This will be achieved by a three-prong approach: (i) Theoretical: by developing a reduced-order flight dynamic model and analyzing the aerodynamics-body-wing-dynamics interactions using geometric control theory and higher-order averaging; (ii) Computational: by solving Navier-Stokes equations around the wings of a flapping insect, coupled with the mechanical equations governing the wing and body motion to study the role of leading and trailing edge vortices in the vibrational stabilization phenomenon; and (iii) Experimental: by building a multi degree-of-freedom test bed (with motion capture and flow visualization) to validate the theoretical and computational findings and experimentally assess the effectiveness of vibrational stabilization in flapping flight and scrutinize its physics. Finally, a new generation of flapping micro-air-vehicles will be developed with minimal actuation, relying on the discovered vibrational stabilization phenomenon.This award reflects NSF's statutory mission and has been deemed worthy of support through evaluation using the Foundation's intellectual merit and broader impacts review criteria.
期刊论文(10)
专著(0)
科研奖励(0)
会议论文
DOI: 10.1016/j.jfluidstructs.2020.102868
发表时间: 2020-02
期刊: Journal of Fluids and Structures
影响因子: 3.6
作者: [Haithem E. Taha;A. Rezaei]
通讯作者: Haithem E. Taha;A. Rezaei
DOI: 10.1088/1748-3190/ac1918
发表时间: 2021-11-01
期刊: BIOINSPIRATION & BIOMIMETICS
影响因子: 3.4
作者: [Mir, Imran, Eisa, Sameh A., Ul Islam, Tauqeer]
通讯作者: Ul Islam, Tauqeer
Feedback Oscillatory Control of Roll Instability During Stall Using the LIBRA Mechanism
使用 LIBRA 机构对失速期间侧倾不稳定性进行反馈振荡控制
DOI: 10.2514/6.2023-1449
发表时间: 2023
期刊: AIAA SciTech
影响因子: --
作者: [Abdelgalil, Mahmoud A., Taha, Haithem E.]
通讯作者: Taha, Haithem E.
DOI: 10.1103/physreve.106.l062401
发表时间: 2022-12-09
期刊: PHYSICAL REVIEW E
影响因子: 2.4
作者: [Abdelgalil, Mahmoud, Aboelkassem, Yasser, Taha, Haithem]
通讯作者: Taha, Haithem
共 10 条
    EAGER/Collaborative Research: Revealing the Physical Mechanisms Underlying the Extraordinary Stability of Flying Insects
    • 批准号:
      2344214
    • 项目类别:
      Standard Grant
    • 资助金额:
      $15.0万
    • 财政年份:
      2024
    • 负责人:
      Haithem Taha
    • 依托单位:
    RAISE: On D'Alembert's Paradox: Can airplanes fly in superfluid?
    • 批准号:
      2332556
    • 项目类别:
      Continuing Grant
    • 资助金额:
      $100.0万
    • 财政年份:
      2023
    • 负责人:
      Haithem Taha
    • 依托单位:
    Viscous Extension of the Classical Theory of Unsteady Aerodynamics
    • 批准号:
      2005541
    • 项目类别:
      Standard Grant
    • 资助金额:
      $30.0万
    • 财政年份:
      2020
    • 负责人:
      Haithem Taha
    • 依托单位:
    EAGER: Revisiting Vibrational Control Theory
    • 批准号:
      1709746
    • 项目类别:
      Standard Grant
    • 资助金额:
      $20.0万
    • 财政年份:
      2017
    • 负责人:
      Haithem Taha
    • 依托单位:
    海外基金