Measurement of boundary-layer transition by towing wind tunnel

Shuya Yoshioka, Yasuaki Kohama, Takuma Kato, Fukuo Ohta, Masahiro Tokuyama, Satoshi Kikuchi

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

    2 Citations (Scopus)

    Abstract

    In this paper a newly constructed Towing wind tunnel facility is introduced. This Towing wind tunnel system can create highly complex flow and zero free stream turbulence condition. The performance of this facility is first explained. The results of our first experiment on the boundary layer transition on a flat plate are then given. We concluded that this facility has good performance for complex flow testing under zero freestream turbulence condition.

    Original languageEnglish
    Title of host publicationICIASF'05 Record - 21st International Congress on Instrumentation in Aerospace Simulation Facilities, 2005
    Pages241-244
    Number of pages4
    Publication statusPublished - 2005 Dec 1
    Event21st International Congress on Instrumentation in Aerospace Simulation Facilities, 2005, ICIASF'05 - Sendai, Japan
    Duration: 2005 Aug 292005 Sep 1

    Publication series

    NameICIASF Record, International Congress on Instrumentation in Aerospace Simulation Facilities
    Volume2005
    ISSN (Print)0730-2010

    Conference

    Conference21st International Congress on Instrumentation in Aerospace Simulation Facilities, 2005, ICIASF'05
    CountryJapan
    CitySendai
    Period05/8/2905/9/1

    ASJC Scopus subject areas

    • Instrumentation
    • Aerospace Engineering
    • Condensed Matter Physics

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  • Cite this

    Yoshioka, S., Kohama, Y., Kato, T., Ohta, F., Tokuyama, M., & Kikuchi, S. (2005). Measurement of boundary-layer transition by towing wind tunnel. In ICIASF'05 Record - 21st International Congress on Instrumentation in Aerospace Simulation Facilities, 2005 (pp. 241-244). [1569929] (ICIASF Record, International Congress on Instrumentation in Aerospace Simulation Facilities; Vol. 2005).