All stabilizing devices increased drag coefficient of right circular cylinder inasmuch as projected frontal area was doubled; conical-flare model only has 30% more drag than cylinder; truncated-cone nose fairings were more effective than circular-arc nose fairings in reducing drag coefficient; pertinence to ballistic missiles.


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    Titel :

    Free-flight measurements of transonic drag characteristics of low-fineness-ratio cylinders including stabilizing plates and flares and varying nose bluntness


    Weitere Titelangaben:

    NASA -- Tech Note


    Beteiligte:
    Judd, J.H. (Autor:in) / Woodbury, G.E. (Autor:in)


    Erscheinungsdatum :

    1960


    Format / Umfang :

    16 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :