Secondary effects in static aeroelasticity that heretofore have been regarded as negligble include: redistribution of induced drag; dihedral effect under load factor; structural axis rotations in equations of motion; aeroelastic divergence of an unrestrained vehicle; and corrections to measurements on 'rigid' wind tunnel model. The few publications on these topics that have appeared over the years are surveyed on the assumption that secondary effects on earlier designs may have become primary effects of future configurations.


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    Title :

    Secondary Considerations of Static Aeroelastic Effects on High-Performance Aircraft


    Contributors:

    Publication date :

    1986


    Size :

    13 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





    Static aeroelastic effects on high-performance aircraft

    Schneider, G. / Zimmermann, H. / Hubschrauber und Flugzeuge, Messerschmitt-Bölkow-Blohm GmbH, Ottobrunn et al. | TIBKAT | 1986




    Some static aeroelastic considerations of slender aircraft

    Hancock, G.J. | Engineering Index Backfile | 1961