Use of jet reaction devicer as means of space vehicle control outside of atmosphere is investigated; ratio of jet stagnation pressure to free stream static pressure was varied from 8 to 460 and jet slot width from 0.001 to 0.05 in.; ratio of aerodynamic to pure jet reaction force was sizable and varied from 0.5 to 9; ratio increased with increasing pressure ratio and decreasing slot width.


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    Titel :

    Aerodynamic interaction effects ahead of sonic jet exhausting perpendicularly from flat-plate into mach number 6 free stream


    Weitere Titelangaben:

    NASA -- Tech Note


    Beteiligte:
    Romeo, D.J. (Autor:in) / Sterrett, J.R. (Autor:in)


    Erscheinungsdatum :

    1961


    Format / Umfang :

    26 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :