Program computes incompressible linear stability characteristics for swept and tapered wings. Amplification rates of boundary-layer disturbances also are calculated. Program is useful in designing tapered, laminar-flow control wings incorporating suction to prevent boundary layer separation. Program is written in FORTRAN IV and Assembler for batch execution on CYBER 70-series.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Disturbance amplification rates


    Contributors:
    Srokowski, A. J. (author) / Orszag, S. A. (author) / Cebech, T. (author) / Kaups, K. (author)

    Published in:

    Publication date :

    1980-08-01



    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English


    Keywords :



    Linear Disturbance Amplification Over Blunted Flat Plates in High-Speed Flows

    Scholten, Anton / Goparaju, Hemanth / Gaitonde, Datta V. et al. | TIBKAT | 2022


    Linear Disturbance Amplification Over Blunted Flat Plates in High-Speed Flows

    Scholten, Anton / Goparaju, Hemanth / Gaitonde, Datta V. et al. | AIAA | 2022