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BASIC RESEARCH ON CAVITATION IN ROCKET PUMP INDUCER

Research Project

Project/Area Number 13650201
Research Category

Grant-in-Aid for Scientific Research (C)

Allocation TypeSingle-year Grants
Section一般
Research Field Fluid engineering
Research InstitutionAKITA NATIONAL COLLEGE OF TECHNOLOGY

Principal Investigator

ITO Jun  AKITA NATIONAL COLLEGE OF TECHNOLOGY, DEPARTMENT OF MECHANICAL ENGINEERING, PROFESSOR, 機械工学科, 教授 (50042312)

Project Period (FY) 2001 – 2002
Project Status Completed (Fiscal Year 2002)
Budget Amount *help
¥500,000 (Direct Cost: ¥500,000)
Fiscal Year 2002: ¥500,000 (Direct Cost: ¥500,000)
KeywordsCAVITATION / CASCADE / INDUCER / ROCKET PUMP / SHEAR FLOW / 理論
Research Abstract

The failure of launching the H II Rocket of 1999 was caused by destruction of turbo-pump due to cavitation occurring in inducer of the pump. Inducer of a rocket pump operates in heavy shear flow due to the walls of casing and boss, and further operates in partially cavitating condition.
From these circumstances, hydrodynamic characteristics are analyzed about a partially cavitating cascade which is placed in shear flow between parallel plane walls.
An equation of motion with respect to disturbance pressure is transformed into two problems by separation of variables. One of them is that of spanwise direction and the other is that of sectional plane of a hydrofoil in cascade.
For the problem of the spanwise direction, an existing analytical solution is adopted. The problem of sectional plane of the hydrofoil in cascade is reduced to a simultaneous integral equation with respect to singularity distributions and is solved by using the analytical method previously proposed by the author for the three dimensional cascade without cavitation.
These two kinds of solutions corresponding to individual eigenvalues are combined linearly, and expression of cascade and cavity characteristics are obtained.
Numerical calculations are carried out to clarify the characteristics, especially cavity free stream line form, for the same cascade condition and cavity length as the real launching condition of H II A Rocket developed newly.

Report

(3 results)
  • 2002 Annual Research Report   Final Research Report Summary
  • 2001 Annual Research Report
  • Research Products

    (21 results)

All Other

All Publications (21 results)

  • [Publications] 伊藤 惇, 他2名: "平行壁間において部分空洞を伴う翼の特性解析"日本機械学会論文集(B). 67-659. 1647-1653 (2001)

    • Description
      「研究成果報告書概要(和文)」より
    • Related Report
      2002 Final Research Report Summary
  • [Publications] 伊藤 惇, 他1名: "指数せん断流中における翼の揚力線理論と超空洞翼への応用"日本機械学会論文集(B). 67-663. 2725-2730 (2001)

    • Description
      「研究成果報告書概要(和文)」より
    • Related Report
      2002 Final Research Report Summary
  • [Publications] 伊藤 惇, 他3名: "せん断流中における三次元翼列の一特異点解法"日本機械学会論文集(B). 68-665. 94-101 (2002)

    • Description
      「研究成果報告書概要(和文)」より
    • Related Report
      2002 Final Research Report Summary
  • [Publications] ITO, Jun, et al.: "Lifting-Line Theory of a Supercavitating Hydrofoil in Two-Dimensional Shear Flow"JSME International Journal, Series B. 45-2. 287-292 (2002)

    • Description
      「研究成果報告書概要(和文)」より
    • Related Report
      2002 Final Research Report Summary
  • [Publications] 伊藤 惇, 他1名: "せん断流中において部分空洞を伴う三次元翼列の理論"ターボ機械. 30-6. 363-373 (2002)

    • Description
      「研究成果報告書概要(和文)」より
    • Related Report
      2002 Final Research Report Summary
  • [Publications] 伊藤 惇, 他1名: "一様せん断流中における翼の揚力線理論と臨界シアパラメータ"日本機械学会論文集(B). 69-679. 547-552 (2003)

    • Description
      「研究成果報告書概要(和文)」より
    • Related Report
      2002 Final Research Report Summary
  • [Publications] 薮 忠司, 伊藤 惇: "数値計算法(機械系教科書シリーズ12)"コロナ社. 170 (2002)

    • Description
      「研究成果報告書概要(和文)」より
    • Related Report
      2002 Final Research Report Summary
  • [Publications] ITO,JUN: "A CHARACTERISTIC ANALYSIS OF PARTIALLY CAVITATING HYDROFOIL BETWEEN PARALLEL PLANE WALLS"TRANS.JSME. 67-659. 1647-1653 (2001)

    • Description
      「研究成果報告書概要(欧文)」より
    • Related Report
      2002 Final Research Report Summary
  • [Publications] ITO,JUN: "LIFTING-LINE THEORY OF A WING IN A SHEAR FLOW AND APPLICATION TO SUPERCAVITATION"TRANS.JSME. 67-663. 2725-2730 (2001)

    • Description
      「研究成果報告書概要(欧文)」より
    • Related Report
      2002 Final Research Report Summary
  • [Publications] ITO,JUN: "A SINGULARITY METHOD FOR THREE-DIMENSIONAL CASCADE IN SHEAR FLOW"TRANS.JSME. 68-665. 94-101 (2002)

    • Description
      「研究成果報告書概要(欧文)」より
    • Related Report
      2002 Final Research Report Summary
  • [Publications] ITO,JUN: "LIFTING-LINE THEORY OF A SUPERCAVITATING HYDROFOIL IN TWO DIMENSIONAL SHEAR FLOW"JSME INTERNATIONAL JOURNAL, SERIES B. 45-2. 287-292 (2002)

    • Description
      「研究成果報告書概要(欧文)」より
    • Related Report
      2002 Final Research Report Summary
  • [Publications] ITO,JUN: "A THEORY OF A THREE-DIMEN-SIONAL CASCADE WITH PARTIAL CAVITATION IN SHEAR FLOW"TURBOMACHINERY. 30-6. 363-373 (2002)

    • Description
      「研究成果報告書概要(欧文)」より
    • Related Report
      2002 Final Research Report Summary
  • [Publications] ITO,JUN: "A LIFTING-LINE THEORY OF A WING AND CRITICAL SHEAR PARAMETER IN UNIFORM SHEAR FLOW"TRANS.JSME. 69-679. 547-552 (2003)

    • Description
      「研究成果報告書概要(欧文)」より
    • Related Report
      2002 Final Research Report Summary
  • [Publications] SOH,TADASHI & ITO,JUN: "METHOD FOR NUMERICAL ANALYSIS (ME CHANICAL ENG. SERIES 12)"KORONA PUBLISHING CO.LTD. 170 (2002)

    • Description
      「研究成果報告書概要(欧文)」より
    • Related Report
      2002 Final Research Report Summary
  • [Publications] 伊藤 惇他2名: "平行壁間において部分空洞を伴う翼の特性解析"日本機械学会論文集,B編. 67・659. 1647-1653 (2001)

    • Related Report
      2002 Annual Research Report
  • [Publications] 伊藤 惇他2名: "せん断流中における三次元翼列の一特異点解法"日本機械学会論文集,B編. 68・665. 94-101 (2002)

    • Related Report
      2002 Annual Research Report
  • [Publications] Jun ITO et al.: "Lifting-Line Theory of a Supercavitating Hydrofoil in Two-Dimensional Shear Flow"JSME International Journal, B. 45・2. 287-292 (2002)

    • Related Report
      2002 Annual Research Report
  • [Publications] 伊藤 惇他1名: "せん断流中において部分空洞を伴う三次元翼列の理論"ターボ機械. 30・6. 363-373 (2002)

    • Related Report
      2002 Annual Research Report
  • [Publications] 藤井大樹他4名: "せん断流中における三次元部分空洞翼列の特性(第2報,解析結果)"秋田高専・研究紀要. 38. 7-12 (2003)

    • Related Report
      2002 Annual Research Report
  • [Publications] 伊藤 惇, 他2名: "平行壁間において部分空洞を伴う翼の特性解析"日本機械学会論文集,B論. 67・659. 1647-1653 (2001)

    • Related Report
      2001 Annual Research Report
  • [Publications] 伊藤 惇, 他2名: "せん断流中における三次元翼列の一特異点解法"日本機械学会論文集,B論. 68・665. 94-101 (2002)

    • Related Report
      2001 Annual Research Report

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Published: 2002-04-01   Modified: 2016-04-21  

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