Rigorous Characterization, Modelling, and Mitigation of Aeroengine Response to Inlet Flow Distortion

航空发动机对进气流量畸变响应的严格表征、建模和缓解

基本信息

  • 批准号:
    RGPIN-2015-06181
  • 负责人:
  • 金额:
    $ 1.6万
  • 依托单位:
  • 依托单位国家:
    加拿大
  • 项目类别:
    Discovery Grants Program - Individual
  • 财政年份:
    2021
  • 资助国家:
    加拿大
  • 起止时间:
    2021-01-01 至 2022-12-31
  • 项目状态:
    已结题

项目摘要

Aeroacoustics; Aircraft engines; Body force models; Boundary layer ingestion; Inlet distortion; Turbomachinery
航空声学;航空发动机;体积力模型;附面层吸入;进气畸变;涡轮机械

项目成果

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会议论文数量(0)
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Defoe, Jeffrey其他文献

Defoe, Jeffrey的其他文献

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{{ truncateString('Defoe, Jeffrey', 18)}}的其他基金

Rigorous Characterization, Modelling, and Mitigation of Aeroengine Response to Inlet Flow Distortion
航空发动机对进气流量畸变响应的严格表征、建模和缓解
  • 批准号:
    RGPIN-2015-06181
  • 财政年份:
    2022
  • 资助金额:
    $ 1.6万
  • 项目类别:
    Discovery Grants Program - Individual
Rigorous Characterization, Modelling, and Mitigation of Aeroengine Response to Inlet Flow Distortion
航空发动机对进气流量畸变响应的严格表征、建模和缓解
  • 批准号:
    RGPIN-2015-06181
  • 财政年份:
    2020
  • 资助金额:
    $ 1.6万
  • 项目类别:
    Discovery Grants Program - Individual
Development of a Simple Air- and O2-Powered Ventilator for Care of COVID-19 Patients
开发用于护理 COVID-19 患者的简单空气和 O2 动力呼吸机
  • 批准号:
    555180-2020
  • 财政年份:
    2020
  • 资助金额:
    $ 1.6万
  • 项目类别:
    Alliance Grants
Numerical investigation of the behaviour of confined, impinging jets with assessment of advanced concepts to reduce unsteady pressure fluctuations in gas turbine testing facilities
对受限冲击射流行为进行数值研究,评估先进概念,以减少燃气轮机测试设施中的不稳定压力波动
  • 批准号:
    520185-2017
  • 财政年份:
    2020
  • 资助金额:
    $ 1.6万
  • 项目类别:
    Collaborative Research and Development Grants
Numerical investigation of the behaviour of confined, impinging jets with assessment of advanced concepts to reduce unsteady pressure fluctuations in gas turbine testing facilities
对受限冲击射流行为进行数值研究,评估先进概念,以减少燃气轮机测试设施中的不稳定压力波动
  • 批准号:
    520185-2017
  • 财政年份:
    2019
  • 资助金额:
    $ 1.6万
  • 项目类别:
    Collaborative Research and Development Grants
Rigorous Characterization, Modelling, and Mitigation of Aeroengine Response to Inlet Flow Distortion
航空发动机对进气流量畸变响应的严格表征、建模和缓解
  • 批准号:
    RGPIN-2015-06181
  • 财政年份:
    2019
  • 资助金额:
    $ 1.6万
  • 项目类别:
    Discovery Grants Program - Individual
Rigorous Characterization, Modelling, and Mitigation of Aeroengine Response to Inlet Flow Distortion
航空发动机对进气流量畸变响应的严格表征、建模和缓解
  • 批准号:
    RGPIN-2015-06181
  • 财政年份:
    2018
  • 资助金额:
    $ 1.6万
  • 项目类别:
    Discovery Grants Program - Individual
Numerical investigation of the behaviour of confined, impinging jets with assessment of advanced concepts to reduce unsteady pressure fluctuations in gas turbine testing facilities
对受限冲击射流行为进行数值研究,评估先进概念,以减少燃气轮机测试设施中的不稳定压力波动
  • 批准号:
    520185-2017
  • 财政年份:
    2018
  • 资助金额:
    $ 1.6万
  • 项目类别:
    Collaborative Research and Development Grants
Rigorous Characterization, Modelling, and Mitigation of Aeroengine Response to Inlet Flow Distortion
航空发动机对进气流量畸变响应的严格表征、建模和缓解
  • 批准号:
    RGPIN-2015-06181
  • 财政年份:
    2017
  • 资助金额:
    $ 1.6万
  • 项目类别:
    Discovery Grants Program - Individual
Rigorous Characterization, Modelling, and Mitigation of Aeroengine Response to Inlet Flow Distortion
航空发动机对进气流量畸变响应的严格表征、建模和缓解
  • 批准号:
    RGPIN-2015-06181
  • 财政年份:
    2016
  • 资助金额:
    $ 1.6万
  • 项目类别:
    Discovery Grants Program - Individual

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