This paper presents an overview of results from the wind tunnel test of a 1/4-scale V-22 proprotor in the Duits-Nederlandse Windtunnel (DNW) in The Netherlands. The small-scale proprotor was tested on the isolated rotor configuration of the Tilt Rotor Aeroacoustic Model (TRAM). The test was conducted by a joint team from NASA Ames, NASA Langley, U.S. Army Aeroflightdynamics Directorate, and The Boeing Company. The objective of the test was to acquire a benchmark database for validating aeroacoustic analyses. Representative examples of airloads, acoustics, structural loads, and performance data are provided and discussed.


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    Titel :

    Overview of the Testing of a Small-Scale Proprotor


    Beteiligte:
    L. A. Young (Autor:in) / G. K. Yamauchi (Autor:in) / J. E. Booth (Autor:in) / G. Botha (Autor:in) / S. Dawson (Autor:in)

    Erscheinungsdatum :

    1999


    Format / Umfang :

    13 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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