课题基金 / 基金详情

Plasma actuation for improved aircraft aerodynamics

Plasma actuation for improved aircraft aerodynamics
等离子驱动可改善飞机空气动力学
批准号:
460936-2013
负责人:
Vo, HuuDuc
金额:
$1.89万
依托单位国家:
加拿大
项目类别:
Collaborative Research and Development Grants
财政年份:
2015
资助国家:
加拿大
项目状态:
已结题
起止时间:
2015-01-01 至 2016-12-31

项目摘要

项目成果

Vo, HuuDuc的其他基金

相似基金

相关文献

中文摘要
翻译
点击翻译按钮获取中文摘要
英文摘要
This research program is a collaboration between researchers in the Department of Mechanical Engineering at École Polytechnique de Montréal and in the Department of Aerospace Engineering at the Indian Institute of Technology-Kanpur (IIT-K). It consists of three projects involving flow control using plasma actuators. Flow control consists of placing relatively low-power actuators at strategic locations to have disproportionally large effects on the flow field. A plasma actuator is a recent electro-fluidic technology capable of converting electricity directly into flow momentum without any moving parts. It does so via partial air ionization through the application of high voltages (but at very low power) between two parallel but offset electrodes separated by a dielectric material. This solid-state, light, thin, simple and purely electrical actuator has high bandwidth and is easy to integrate thus offering the first practical widespread use of flow control to potentially revolutionize aircraft aerodynamics. The first project of the research aims to delay laminar-turbulent boundary layer transition on aircraft surfaces with plasma actuators in order to reduce viscous drag. The second project will investigate the control of boundary layer separation on airfoils at high angles of attack to increase the effectiveness of airfoil flaps in the short term and eventually to remove wing flaps, slats and spoilers altogether. The third project is to develop two new concepts to change lift on wings and empenages at low angles of attack with well-attached boundary layers via modification of the wing tip vortex and trainling edge flow curvature with plasma actuators in order to eliminate all movable flight control surfaces. École Polytechnique de Montréal will be responsible for setting up and carrying out all wind tunnel validation experiments in all three projects as well as some numerical simulations in project 3 while IIT-K will be responsible for all computational work in projects 1 and 2 and part of project 3.
期刊论文(0)
专著(0)
科研奖励(0)
会议论文
Innovative Compressor/Fan Technologies for Reduction of Fossil Fuel Consumption
  • 批准号:
    RGPIN-2022-04752
  • 项目类别:
    Discovery Grants Program - Individual
  • 资助金额:
    $1.97万
  • 财政年份:
    2022
  • 负责人:
    Vo, HuuDuc
  • 依托单位:
Aerodynamic Improvement of Centrifugal Compressors
  • 批准号:
    RGPIN-2016-06645
  • 项目类别:
    Discovery Grants Program - Individual
  • 资助金额:
    $1.89万
  • 财政年份:
    2021
  • 负责人:
    Vo, HuuDuc
  • 依托单位:
Aerodynamic Improvement of Centrifugal Compressors
  • 批准号:
    RGPIN-2016-06645
  • 项目类别:
    Discovery Grants Program - Individual
  • 资助金额:
    $1.89万
  • 财政年份:
    2020
  • 负责人:
    Vo, HuuDuc
  • 依托单位:
Aerodynamic Improvement of Centrifugal Compressors
  • 批准号:
    RGPIN-2016-06645
  • 项目类别:
    Discovery Grants Program - Individual
  • 资助金额:
    $1.89万
  • 财政年份:
    2019
  • 负责人:
    Vo, HuuDuc
  • 依托单位:
海外基金