Method for calculation of aerodynamic forces on oscillating combination of wing and fin is described; method is based on linearized theory and constitutes extension of method previously developed for isolated finite wings, indexed in Engineering Index 1959 p 24; results are given for 3 particular rigid modes and for Mach numbers 0 and 0.8.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Aerodynamic forces on combination of wing and fin oscillating in subsonic flow


    Additional title:

    Svenska Aeroplan Aktiebolaget -- Tech Note


    Contributors:


    Publication date :

    1964


    Size :

    36 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :