A number of theoretical investigations have been conducted in the development of the design and analysis of advanced propeller configurations. Lock and Theodorsen as described by Davidson have been utilized to study counterrotating propeller systems. A different numerical method known as “SSTAGE”, which is an Euler solver for the Unducted Fan (UDF) concept, was used to predict the acoustic near field that compared well with experimental data. The NASPROP-E numerical analysis also consisting of an Euler solver has been used to theoretically study the near acoustic fields for the SR series propfan configurations. A counterrotating propeller test rig (CRPTR) was designed and built to obtain an experimental performance/acoustic data base for various propeller configurations for means of comparison with theoretical predictions.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Application of Computational Aeroacoustic Methodologies to Advanced Propeller Configurations - A Review


    Additional title:

    Sae Technical Papers


    Contributors:

    Conference:

    General, Corporate & Regional Aviation Meeting & Exposition ; 1991



    Publication date :

    1991-04-01




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




    Application of computational aeroacoustic methodologies to advanced propeller configurations - A review

    Korkan, K.D. / Eagleson, L.A. / Griffiths, R.C. | Tema Archive | 1991


    Propeller aeroacoustic methodologies

    Korkan, K. D. / Gregorek, G. M. | NTRS | 1980


    Comparison of Various Aeroacoustic Propeller Noise Prediction Methodologies in Static Operations

    Bergmann, Ole / Möhren, Felix / Braun, Carsten et al. | AIAA | 2022