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A Study of Engineering Application of Pulsed Vortex Generator Jet

Research Project

Project/Area Number 11450080
Research Category

Grant-in-Aid for Scientific Research (B).

Allocation TypeSingle-year Grants
Section一般
Research Field Fluid engineering
Research InstitutionScience University of Tokyo

Principal Investigator

HONAMI Shinji  Science University of Tokyo, Faculty of Engineering, Professor, 教授 (30089312)

Project Period (FY) 1999 – 2000
Project Status Completed (Fiscal Year 2000)
Budget Amount *help
¥6,000,000 (Direct Cost: ¥6,000,000)
Fiscal Year 2000: ¥2,200,000 (Direct Cost: ¥2,200,000)
Fiscal Year 1999: ¥3,800,000 (Direct Cost: ¥3,800,000)
KeywordsFlow separation / Reattaching flow / Vortex generator jet / Flow control / Close loop control / Pulsed jet / Backward facing step flow / 乱流境界層 / 渦発生ジエット / パルスジエット / 再付着過程 / 能動制御 / マイクロセンサ
Research Abstract

The general goal of the present study is to construct the closed loop control system of the reattachment process in a backward facing step flow by a row of the pulsed vortex generator jets. The step height is 40 mm. An expansion ratio of the test section height to the step height is 1.5. The step height Reynolds number is 2.7×10^4. The vortex generator jets are injected through a row of the 2 mm diameter injection holes. A micro wall flow sensor, which can detect near-wall flow reversal with a frequency response up to 500 Hz, measures time fraction of forward and backward flow. The reattachment line is almost parallel to the span-wise direction in the range of the hole pitch ratio of 10 to 20, although the discrete disturbance by jet injection is provided at the step. The reattachment length is decreased linearly up to the velocity ratio of 6. This means that the velocity ratio is one of the most effective manipulated variables in the control system of the reattachment process. The wall static pressure in the reattachment region is selected as the control feedback signal and the velocity ratio is used as the manipulated variable in the control system. The faster response of the system with the time constant of an order of 0.1 second is obtained. As a result, the present system can be employed in the engineering application as the effective control system for flow separation.

Report

(3 results)
  • 2000 Annual Research Report   Final Research Report Summary
  • 1999 Annual Research Report
  • Research Products

    (9 results)

All Other

All Publications (9 results)

  • [Publications] 伊藤智仁,本阿弥眞治 他1名: "パルス渦発生ジェットに関する研究"日本機械学会論文集B編. 66・644. 985-989 (2000)

    • Description
      「研究成果報告書概要(和文)」より
    • Related Report
      2000 Final Research Report Summary
  • [Publications] 森岡禎,本阿弥眞治: 日本機械学会論文集B編. 67・656(印刷中). (2001)

    • Description
      「研究成果報告書概要(和文)」より
    • Related Report
      2000 Final Research Report Summary
  • [Publications] 中嶋秀成,本阿弥眞治 他4名: 日本機械学会論文集B編. 67・655. 589-594 (2001)

    • Description
      「研究成果報告書概要(和文)」より
    • Related Report
      2000 Final Research Report Summary
  • [Publications] T.Itoh, S.Honami et al.: "A study of pulsed vortex generator jet"Transactions of JSME, Ser B. Vol.66, No 644. 985-989 (2000)

    • Description
      「研究成果報告書概要(欧文)」より
    • Related Report
      2000 Final Research Report Summary
  • [Publications] T.Morioka & S.Honami: "A closed loop control system of a backward-facing step flow by a vortex generator jet"Transactions of JSME, Ser B. Vol.67, No 656 (in press). (2001)

    • Description
      「研究成果報告書概要(欧文)」より
    • Related Report
      2000 Final Research Report Summary
  • [Publications] H.Nakajima, S.Honami et al.: "Behavior of thermal and fluid flow around a micro-sensor"Transactions of JSME, Ser B. Vol.67, No 655. 589-594 (2001)

    • Description
      「研究成果報告書概要(欧文)」より
    • Related Report
      2000 Final Research Report Summary
  • [Publications] 伊藤智仁,志澤高朗,本阿弥眞治: "パルス渦発生ジェットに関する研究"日本機械学会論文集 B編. 66・644. 985-989 (2000)

    • Related Report
      2000 Annual Research Report
  • [Publications] 森岡禎,本阿弥眞治: "渦発生ジェットによる後方ステップ流れの閉ループ制御"日本機械学会論文集 B編. (掲載予定). (2001)

    • Related Report
      2000 Annual Research Report
  • [Publications] T.Morioka & S.Honami: "A Control System of Backward Facing Step Flow by Vortex Generator Jets"AIAA(米国航空宇宙学会)(2001.6米国アナハイム). (発表予定). (2001)

    • Related Report
      2000 Annual Research Report

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Published: 1999-04-01   Modified: 2016-04-21  

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