Concept of maneuver margin is discussed, and definitions are suggested which are applicable to all types of configurations; calculations are presented for maneuver characteristics of simplified flexible models representing conventional and slender integrated aircraft.


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    Title :

    Static aeroelastic deformation of slender configurations -- 4. Manoeuvre theory


    Additional title:

    Aeronautical Quarterly


    Contributors:

    Published in:

    Publication date :

    1963


    Size :

    20 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    MANOEUVRE-LOADS COMPUTATIONS USING CFD-BASED STATIC AEROELASTIC SIMULATIONS FOR MULTIPLE STORE CONFIGURATIONS

    Prananta, B.B. / Veul, R.P.G. / Boelens, O.J. et al. | British Library Conference Proceedings | 2010


    Some static aeroelastic considerations of slender aircraft

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