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Investigations for Flow Around slender bodies at high angles of attack

Research Project

Project/Area Number 60460074
Research Category

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

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

Principal Investigator

KUBOTA Hirotoshi  Department of Aeronautics, Faculty of Engineering, University of Tokyo, 工学部, 教授 (30114466)

Co-Investigator(Kenkyū-buntansha) WATANUKI Tadaharu  Department of Aeronautics, Faculty of Engineering, University of Tokyo, 工学部, 助手 (00182965)
MATSUZAKA Masayoshi  Department of Aeronautics, Faculty of Engineering, University of Tokyo, 工学部, 助手 (00010900)
Project Period (FY) 1985 – 1986
Project Status Completed (Fiscal Year 1986)
Budget Amount *help
¥6,700,000 (Direct Cost: ¥6,700,000)
Fiscal Year 1986: ¥2,400,000 (Direct Cost: ¥2,400,000)
Fiscal Year 1985: ¥4,300,000 (Direct Cost: ¥4,300,000)
KeywordsSlender body / Flow around high-angle-of-attack body / Vortex; Separated flow / Wind tunnel testing / Flow visualization / Navier-Stokes equation / ナヴィエ・ストークス方程式 / 数値シミュレーション
Research Abstract

Investigations for flow around the slender bodies at high angles of attack and the related aerodynamic characteristics are carried out with the use of both the flow visualization/force measurements in the low speed wind tunnel and the numerical simulation.
The major conclusions are as follows:
1. Flow around the axisymmetric bodies shows the asymmetries at angles of attack of 60-75 deg and it causes the asymmetric side force.
2. The empirical law that "the nonlinear aerodynamic characteristics appears at angle of attack as approximately twice as cone angle of body" which is effective to axisymmetric body can be also applied to the non-axisymmetric bodies.
3. When the foreplane is attached on the slender body, it somewhat alleviates the occurrence of asymmetric side force and demonstrates the possibility of application to lateral control of space transportation system.
4. Flow structure and aerodynamic characteristics can be simulated in some extent with the Navier-Stokes analysis. The structures of the three-dimensional separated flow (nodes, foci, saddles, etc.) can be numerically obtained based on the computational results of Navier-Stokes equations.

Report

(1 results)
  • 1986 Final Research Report Summary
  • Research Products

    (6 results)

All Other

All Publications (6 results)

  • [Publications] 久保田弘敏,松坂正芳,綿貫忠晴,鈴木宏二郎: 15th International Symposium on Space Technology and Science(第15回国際宇宙技術と科学のシンポジウム)論文集. 593-598 (1986)

    • Description
      「研究成果報告書概要(和文)」より
    • Related Report
      1986 Final Research Report Summary
  • [Publications] 加茂圭介,久保田弘敏,姫野龍太郎,桑原邦郎: AIAA(アメリカ航空宇宙学会)Paper 86-1778-CP. 86-96 (1986)

    • Description
      「研究成果報告書概要(和文)」より
    • Related Report
      1986 Final Research Report Summary
  • [Publications] 鈴木宏二郎,松坂正芳,綿貫忠晴,井戸田典彦,久保田弘敏: International Conference on Fluid Mechanics,Beijing(北京国際流体力学会議)論文集. (1987)

    • Description
      「研究成果報告書概要(和文)」より
    • Related Report
      1986 Final Research Report Summary
  • [Publications] Kubota, H., Matsuzaka, M., Watanuki, T. and Suzuki, K.: "Experimental Investigation of Separated Flow Around High-Angle-of-Attack Slender Bodies" Proc. of 15th International Symposium on Space Technology and Science, Tokyo. 593-598 (1986)

    • Description
      「研究成果報告書概要(欧文)」より
    • Related Report
      1986 Final Research Report Summary
  • [Publications] Kamo, K., Kubota, H., Himeno, R. and Kuwahara, K.: "Computational Simulation of the Flow around a Rocket Body at High Angle of Attack" AIAA Paper 86-1778-CP. 86-96 (1986)

    • Description
      「研究成果報告書概要(欧文)」より
    • Related Report
      1986 Final Research Report Summary
  • [Publications] Suzuki, K., Matsuzaka, M., Watanuki, T., Itoda, N. and Kubota, H.: "Singular Aerodynamic Features of Low-Speed High-Angles-of-Attack Slender Bodies" Proc. of International Conference on Fluid Mechanics, Beijing (to be published). (1987)

    • Description
      「研究成果報告書概要(欧文)」より
    • Related Report
      1986 Final Research Report Summary

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Published: 1987-03-31   Modified: 2016-04-21  

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