Characteristics of wings of high aspect ratio experiencing bending and torsional deformations, calculated for supersonic speed by application of linearized lifting surface theory; calculations for wing of aspect ratio 3.2 and 60° sweepback are presented for Mach number 1.414 and for incompressible flow.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Longitudinal stability of elastic swept wings at supersonic speed


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:
    Frick, C.W. (author) / Chubb, R.S. (author)


    Publication date :

    1949


    Size :

    38 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English




    Longitudinal stability of elastic swept wings at supersonic speed

    Frick, C.W. / Chubb, R.S. | Engineering Index Backfile | 1950


    Longitudinal stability of elastic swept wings at supersonic speed

    Frick, C.W. / Chubb, R.S. | Engineering Index Backfile | 1950




    Swept wings in supersonic flight

    Gates, S. B. | TIBKAT | 1954