• Search Research Projects
  • Search Researchers
  • How to Use
  1. Back to previous page

Unsteady Behavior of a Tip Vortex and Its Effect on the Unsteady Aerodynamic Force of a Downstream Blade

Research Project

Project/Area Number 06651065
Research Category

Grant-in-Aid for General Scientific Research (C)

Allocation TypeSingle-year Grants
Research Field Aerospace engineering
Research InstitutionUniversity of Tokyo

Principal Investigator

WATANABE Toshinori  Univ.of Tokyo, Dept.of Aero.& Astro., Associate Professor, 大学院・工学系研究科, 助教授 (10201211)

Project Period (FY) 1994 – 1995
Project Status Completed (Fiscal Year 1995)
Budget Amount *help
¥2,300,000 (Direct Cost: ¥2,300,000)
Fiscal Year 1995: ¥300,000 (Direct Cost: ¥300,000)
Fiscal Year 1994: ¥2,000,000 (Direct Cost: ¥2,000,000)
KeywordsTurbomachinery / Cascade Flow / Unsteady Internal Flow / Tip Clearance / Tip Leakage Flow / Tip Vortex / Unsteady Aerodynamic Force / ターボ機械 / 翼列干渉 / 振動翼列
Research Abstract

Unsteady behavior of a tip leakage vortex affected by periodic gust, and the one generated from an oscillating blade, were experimentally studied with a three-sensor hot-wire anemometer.The experiment was conducted in a low-speed wind tunnel in which a blade was set with a clearance between its tip and the tunnel wall.The periodic gust from rotating cylinders was introduced to the blade, and the three dimensional flow velocities were measured at downstream positions.When the wake reached the blade leading edge, the tip vortex was observed to diminish, and then it gradually regained the vorticity.The vortex center was found to oscillate with a large amplitude in the direction of blade thickness.It was thus clarified that the tip vortex was quite strongly affected by the incoming gust.The tip vortex generated from an oscillating blade was then detected by the hot-wire anemometry.The in-phase oscillation of the tip vortex with the blade oscillation was clearly observed.The change in the phase of the vortex oscillation in the downstream direction could be explained by the convection of the vortex due to mean flow.In the final stage, the unsteady pressure distributions were measured on a flat plate set at a downstream position of the oscillating blade, The surface pressure substantially decreased due to the passage of the oscillating tip vortex, and, thereby, the unsteady aerodynamic force on the flat plate was significantly changed.When the tip vortex moved across the flat plate, its position changed widely in the spanwise direction.The unsteady pressure field was accordingly changed in a wide area in the spanwise direction.A theoretical study was performed at the same time, in which a new singularity method was developed to estimate the induced unsteady aerodynamic force by the unsteady tip vortex with arbitrary vorticity and position.

Report

(3 results)
  • 1995 Annual Research Report   Final Research Report Summary
  • 1994 Annual Research Report
  • Research Products

    (3 results)

All Other

All Publications (3 results)

  • [Publications] 渡辺紀徳: "翼端間隙流れの構造と翼端渦の非定常挙動" 日本航空宇宙学会第36回航空動機・宇宙推進講演会講演集. 178-183 (1996)

    • Description
      「研究成果報告書概要(和文)」より
    • Related Report
      1995 Final Research Report Summary
  • [Publications] Watanabe Toshinori: ""Tip Clearance Flow Structure and Unsteady Behavior of Tip Vortex, "" Proceedings of the 36th Conference on Aerospace Propulsion. 178-183 (1996)

    • Description
      「研究成果報告書概要(欧文)」より
    • Related Report
      1995 Final Research Report Summary
  • [Publications] 渡辺紀徳: "翼端間隙流れの構造と翼端渦の非定常挙動" 第36回航空原動機・宇宙推進講演会講演集. 178-183 (1996)

    • Related Report
      1995 Annual Research Report

URL: 

Published: 1994-04-01   Modified: 2016-04-21  

Information User Guide FAQ News Terms of Use Attribution of KAKENHI

Powered by NII kakenhi