VARIATION IN “TYPICAL VALUE” PARAMETERS IT has previously been shown that the effect of freeing the controls on the lateral stability of an aircraft may be taken account of by changes both in the values of the derivatives lp, lr, np and nr (wing), which hitherto have had typcial values, and also of the variables x, y and t themselves. It is therefore desirable to have information on the effect on the stability boundaries of changes in these derivatives. It may also happen that the values of yv and tan Θo in the case of a particular aircraft may be known to differ from those here adopted in the drawing of stability charts. The versatility of these charts (later to be given) will therefore be considerably increased if rules are expounded for assessing the effects of changes in any of those derivatives which were formerly fixed. This we proceed to do.


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    Title :

    The Lateral Stability of Aeroplanes


    Subtitle :

    A New Geometrical System of Analysis


    Contributors:
    Price, H.L. (author)

    Published in:

    Publication date :

    1943-09-01


    Size :

    6 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English



    Lateral stability of aeroplanes

    Price, H.L. | Engineering Index Backfile | 1943


    Lateral stability in aeroplanes

    Levick, C. | Engineering Index Backfile | 1918


    The Lateral Stability of Aeroplanes

    Price, H.L. | Emerald Group Publishing | 1943


    The Lateral Stability of Aeroplanes

    Price, H.L. | Emerald Group Publishing | 1943


    The Lateral Stability of Aeroplanes

    Price, H.L. | Emerald Group Publishing | 1943