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MRI: Development of a Next Generation Polysonic Wind Tunnel for Transformative Active Control Technologies and Non-Intrusive Flow Diagnostics

MRI: Development of a Next Generation Polysonic Wind Tunnel for Transformative Active Control Technologies and Non-Intrusive Flow Diagnostics
MRI:开发下一代多声波风洞,用于变革性主动控制技术和非侵入式流量诊断
批准号:
1039825
负责人:
Farrukh Alvi
金额:
$329.5万
依托单位:
依托单位国家:
美国
项目类别:
Standard Grant
财政年份:
2010
资助国家:
美国
项目状态:
已结题
起止时间:
2010-09-01 至 2015-12-31

项目摘要

项目成果

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中文摘要
翻译
这个主要研究仪器(MRI)开发项目是一个新的多晶硅风洞排污设施,由压缩空气产生和储存系统、测试部分和排气系统组成。风洞的典型特征是其速度范围和测试部分的大小。该设施的测试部分为12英寸x 12英寸x 24英寸,马赫数范围为0.2至5,最大雷诺数能力约为2000万/英尺。这个设施将大到足以对工业有用,确保其长期有效使用,但小到足以在大学有效地运作。它将用于开发创新的、实用的主动流量和噪声控制技术以及先进的诊断技术,以研究高速飞行器的设计和基本问题。它将结合独特的设计特点,具有低测试段噪声和广泛的流体诊断光学通道。多晶硅风洞将创造一个独特的共享资源,a)在气体动力学、材料科学和其他领域取得根本性进展;B)发展变革性的流量控制技术;c)吸引、教育并帮助留住多样化的工程师和科学家,包括我们合作机构中代表性不足的少数族裔。因此,该设施将产生关键知识,同时大大加速导致下一代设计的变革性研究。它还将利用和增加佛罗里达先进航空推进中心的资源,这是一个由佛罗里达州立大学领导的多所大学全州卓越中心。
英文摘要
This Major Research Instrumentation (MRI) development project is for a new polysonic wind tunnel blowdown facility consisting of a compressed air generation and storage system, test sections, and exhaust system. A wind tunnel is typically characterized by its speed range and the size of its test section. The facility has a 12-in x 12-in x 24-in test section with a Mach number range of 0.2 to 5 with a maximum Reynolds number capability of roughly 20 million/foot. This facility will be large enough to be useful to industry, ensuring its long-term, efficient use but small enough to be efficiently operated in a university. It will be used to develop innovative, practical active flow and noise control techniques and advanced diagnostics to study the design of, and fundamental problems in, high-speed flight vehicles. It will incorporate unique design features with low test-section noise and extensive optical access for flow diagnostics. The PolySonic Wind Tunnel will create a unique shared resource to a) produce fundamental advances in gas dynamics, material science and other areas; b) develop transformational flow control technologies; and c) attract, educate, and help retain a diverse pool of engineers and scientists, including underrepresented minorities from our partner institutions. The facility will thus produce critical knowledge while dramatically accelerating transformative research leading to next-generation designs. It will also leverage and augment the resources of the Florida Center for Advanced Aero-Propulsion, a multi-university, statewide Center of Excellence, led by Florida State University.
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会议论文
UNS: A Collaborative Approach to Exploring Control Strategies Based on Optimally-Growing Disturbances for Complex Flows
  • 批准号:
    1510919
  • 项目类别:
    Continuing Grant
  • 资助金额:
    $32.38万
  • 财政年份:
    2015
  • 负责人:
    Farrukh Alvi
  • 依托单位:
国内基金
海外基金
水稻边界发育缺陷突变体abnormal boundary development(abd)的基因克隆与功能分析
Development of a Linear Stochastic Model for Wind Field Reconstruction from Limited Measurement Data
  • 批准号:
    --
  • 项目类别:
    --
  • 资助金额:
    40万元
  • 批准年份:
    2020
  • 负责人:
    Vikrant Gupta
  • 依托单位: