Static longitudinal stability and control, and lateral characteristics of model were measured; modifications to model for reducing drag were forward fuselage additions and special wing bodies; components and changes investigated included empennage, wing tip body, wing fences, wing trailing edge flaps, horizontal tail settings, and wing dihedral angle.


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    Title :

    Wind-tunnel investigation of transonic-transport configuration utilizing drag-reducing devices at mach numbers from 0.20 to 1.03


    Additional title:

    NASA -- Tech Note


    Contributors:


    Publication date :

    1961


    Size :

    117 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :