Wind-tunnel research program has been designed to show effects on longitudinal stability and control of several configuration variables; results to date do not allow formulation of general design rules, but effects of several configuration variables have been noted to have prime influence on post-stall characteristics; increase in tail size, changes in location of fuselage-mounted engine nacelles, and reduced fuselage-forebody lift were found to have beneficial effect on static longitudinal stability at high angles of attack.


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    Title :

    Deep-stall aerodynamic characteristics of T-tail aircraft


    Additional title:

    NASA SP


    Contributors:
    Taylor, R.T. (author) / Ray, E.J. (author)

    Published in:

    Publication date :

    1965


    Size :

    9 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :


    Deep-stall aerodynamic characteristics of t-tail aircraft

    Ray, E. J. / Taylor, R. T. | NTRS | 1965


    Deep-Stall Aerodynamic Characteristics of T-Tail Aircraft

    Taylor, Robert T. / Ray, Edward J. | NTRS | 1965


    The deep-stall problem of T-tail aircraft.

    Polhamus, E. C. | NTRS | 1966