Viscous Extension of the Classical Theory of Unsteady Aerodynamics
Viscous Extension of the Classical Theory of Unsteady Aerodynamics
批准号:
2005541
负责人:
Haithem Taha
金额:
$30.0万
依托单位国家:
美国
项目类别:
Standard Grant
财政年份:
2020
资助国家:
美国
项目状态:
已结题
起止时间:
2020-05-15 至 2024-04-30
中文摘要
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英文摘要
The current state-of-the-art of fluid dynamic models of the flow over wing sections are either computationally too expensive to be used in preliminary design phases or overly simplified, neglecting some essential physics. The objective of this proposal is to fill this gap by developing efficient aerodynamic models that capture the main physics of the flow dynamics. Relying on a unique combination of the fundamental knowledge of basic unsteady aerodynamics and the recent advances in data science (for example, machine learning techniques), this project will yield more realistic computations of the aerodynamic loads. The developed theory will be indispensable for preliminary design of next generation flying vehicles (flying taxis, micro-air-vehicles, and drones) and wind turbines, which will improve national security and economic prosperity. The project will include the development of a graduate course on unsteady aerodynamics based on this research, plans are underway to develop a textbook on the subject, and undergraduate students will be involved byway of aerodynamic-related senior projects.Realizing that the lift generation and vorticity production are essentially viscous processes, a viscous extension of the classical theory of unsteady aerodynamics is proposed. This extension will be achieved by coupling the potential theory with a special boundary layer theory that resolves the flow details in the vicinity of the trailing edge. This approach will provide the circulation dynamics without any need for an auxiliary condition (i.e., Kutta-like condition). Moreover, to generalize this approach, machine learning tools will be employed to extract information about the circulation dynamics from high-fidelity simulations. This modeling approach can be conceptually described by a bow tie architecture: a compressive mapping taking a high-dimensional input space (e.g., flow field from high-fidelity simulation) to a smaller, more compact lower-dimensional core model (e.g., one-dimensional circulation dynamics). Then, the potential flow theory, with the accurate circulation dynamics, will be used to recover a high-dimensional output space of the flow field.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.
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Static and Dynamic Characteristics of the Aerodynamic Forces on Pitching Airfoils between 0 to 360 degrees Angle of Attack
0~360°迎角俯仰翼型气动力的静动态特性
DOI:
10.2514/6.2022-1663
发表时间:
2022
期刊:
AIAA SciTech
影响因子:
--
作者:
[Fouda, Moatasem, Khalifa, Nabil M., Rashad, Mahmoud M., Shao, Mingdong, Elsharif, Mostafa, Taha, Haitham E.]
通讯作者:
Taha, Haitham E.
DOI:
10.2514/6.2021-1830
发表时间:
2020-01
期刊:
AIAA Scitech 2021 Forum
影响因子:
--
作者:
[H. Taha;A. Rezaei]
通讯作者:
H. Taha;A. Rezaei
Circulation dynamics of small-amplitude pitching airfoil undergoing laminar-to-turbulent transition
经历层流到湍流转变的小幅度俯仰翼型的环流动力学
DOI:
10.1016/j.jfluidstructs.2020.103177
发表时间:
2021
期刊:
Journal of Fluids and Structures
影响因子:
3.6
作者:
[Rezaei, Amir S., Taha, Haithem]
通讯作者:
Taha, Haithem
Compressible Unsteady Aerodynamic Loads on Oscillating Airfoils in a Subsonic Flow
亚音速流中振荡翼型的可压缩非定常气动载荷
DOI:
10.2514/6.2022-1980
发表时间:
2022
期刊:
AIAA SciTech
影响因子:
--
作者:
[El-Nadi, Ahmed I., Khalifa, Nabil M., Taha, Haitham E.]
通讯作者:
Taha, Haitham E.
DOI:
10.1017/jfm.2022.348
发表时间:
2021-04
期刊:
Journal of Fluid Mechanics
影响因子:
3.7
作者:
[Cody Gonzalez;Haithem E. Taha]
通讯作者:
Cody Gonzalez;Haithem E. Taha
共 7 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:
CAREER: Investigation of Dynamic Interactions Between Wing-Body and Aerodynamics in Bio-Inspired Flight
-
批准号:1846308
-
项目类别:Standard Grant
-
资助金额:$50.0万
-
财政年份:2019
-
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:
Collaborative Research: Unsteady Hydrodynamics and Geometric Control of Pisciform Locomotion
-
批准号:1635673
-
项目类别:Standard Grant
-
资助金额:$18.0万
-
财政年份:2016
-
负责人:Haithem Taha
-
依托单位:
海外基金