The purpose of the evaluation was (1) to measure the acoustic noise environment in the cockpit of the United Kingdom Hawker Siddeley P-1127 V/STOL aircraft that would serve as an acoustic guideline for cockpit noise levels of aircraft being contemplated or under construction, and (2) to determine the acoustic attenuation of various Air Force flight helmets in the inventory or being contemplated for Air Force inventory items. Cockpit sound pressure levels in the P-1127 V/STOL aircraft at various engine rpm settings were measured. The cockpit noise environment at maximum engine rpm was reproduced in the laboratory and used to obtain objective attenuation data for three Air Force flight helmet/liner configurations. Measurement of real-ear attenuation at threshold were also accomplished on the helmet/liner configurations. (Author)


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    Title :

    Noise Environs and Helmet Performance for the P-1127 V/STOL Aircraft


    Contributors:
    H. C. Sommer (author) / J. F. Rose (author) / W. C. Knoblach (author)

    Publication date :

    1968


    Size :

    29 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Noise Environs and Helmet Performance for the P-1127 V/STOL Aircraft

    H. Sommer / J. F. Rose / W. C. Knoblach | NTIS | 1968


    Hawker Siddeley P.1127 V/STOL Strike Reconnaissance Aircraft

    Crampton, J. / Lickley, R. L. | SAE Technical Papers | 1964


    Hawker-Siddeley P.1127 V/STOL. Strike reconnaissance aircraft

    Lickley, R.L. / Crampton, J. | Engineering Index Backfile | 1964



    Nr. 1127

    DataCite | 1867

    Free access