Interior noise ground tests conducted on a DC-9 aircraft test section are described. The objectives were to study ground test and analysis techniques for evaluating the effectiveness of interior noise control treatments for advanced turboprop aircraft, and to study the sensitivity of the ground test results to changes in various test conditions. Noise and vibration measurements were conducted under simulated advanced turboprop excitation, for two interior noise control treatment configurations. These ground measurement results were compared with results of earlier UHB (Ultra High Bypass) Demonstrator flight tests with comparable interior treatment configurations. The Demonstrator is an MD-80 test aircraft with the left JT8D engine replaced with a prototype UHB advanced turboprop engine.


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    Titel :

    Analysis of interior noise ground and flight test data for advanced turboprop aircraft applications


    Beteiligte:
    Simpson, M. A. (Autor:in) / Tran, B. N. (Autor:in)

    Erscheinungsdatum :

    1991-08-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :



    Interior Noise Control Ground Test Studies for Advanced Turboprop Aircraft Applications

    M. A. Simpson / M. R. Cannon / P. L. Burge et al. | NTIS | 1989


    Interior noise control ground test studies for advanced turboprop aircraft applications

    Simpson, Myles A. / Cannon, Mark R. / Burge, Paul L. et al. | NTRS | 1989


    Comparison of Advanced Turboprop Interior Noise Control Ground and Flight Test Data

    Simpson, M. A. / Tran, B. N. / Deutsche Gesellschaft fur Luft- und Raumfahrt e.V. et al. | British Library Conference Proceedings | 1992