During the period September 1997 to February 1998, the Tupolev 144 Supersonic Flyine Laboratory was used to obtain data for the purpose of enlarging the data base used by models for the prediction of cabin noise in supersonic passenger airplanes. Measured were: turbulent boundary layer pressure fluctuations on the fuselage in seven instrumented window blanks distributed over the length of the fuselage; structural response with accelerometers on skin panels close to those window blanks-, interior noise with microphones at the same fuselage bay stations as those window blanks. Flight test points were chosen to cover much of the TU- 144's flight envelope, as well as to obtain as large a unit Reynolds number range as possible at various Mach numbers: takeoff, landing, six subsonic cruise conditions, and eleven supersonic conditions up to Mach 2. Engine runups and reverberation times were measured with a stationary aircraft. The data in the form of time histories of the acoustic signals, together with auxiliary data and basic MATLAB processing modules, are available on CD-R disks.


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    Title :

    Flight Test Measurements From The Tu- 144LL Structure/Cabin Noise Experiment


    Contributors:
    S. A. Rizzi (author) / R. G. Rackl (author) / E. V. Andrianov (author)

    Publication date :

    2000


    Size :

    206 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Flight Test Measurements From The Tu- 144LL Structure/Cabin Noise Experiment

    Rizzi, Stephen A. / Rackl, Robert G. / Andrianov, Eduard V. | NTRS | 2000


    Flight Test Measurements From The Tu-144LL Structure/Cabin Noise Follow-On Experiment

    S. A. Rizzi / R. G. Rackl / E. V. Andrianov | NTIS | 2000


    Flight Test Measurements From The Tu-144LL Structure/Cabin Noise Follow-On Experiment

    Rizzi, Stephen A. / Rackl, Robert G. / Andrianov, Eduard V. | NTRS | 2000