A wind tunnel test of a one-thirtieth scale 'B' series Atlas missile with operating rocket engines was run at the NACA Lewis 8-by-6 foot supersonic wind tunnel. The primary test objective was to determine the amount of rocket and gas turbine exhaust recirculation into the missile base region; a secondary objective was to determine the effect of operating rockets on missile skin and base pressure. Only the pressure data are considered in this report. (Author)


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    Titel :

    A Preliminary Analysis of Rocket Exhaust Jet Effects on Missile Skin and Base Pressures at Mach 0.6 and 1.5 - Naca Lewis Flight Propulsion Laboratory Test 2093


    Beteiligte:
    G. E. Powell (Autor:in)

    Erscheinungsdatum :

    1958


    Format / Umfang :

    16 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch