Rocket powered delta wing aircraft tested had small horizontal tail mounted behind and above exit of rocket nozzle; results indicated that model encountered large jet induced effects on longitudinal trim believed to result from fact that horizontal tail either intersected or was very close behind shock wave in external flow originating near intersection of external flow and jet boundary.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Jet effects on longitudinal trim of airplane configuration measured at mach numbers between 1.2 and 1.8


    Weitere Titelangaben:

    NASA -- Tech Note


    Beteiligte:
    Peck, R.F. (Autor:in)


    Erscheinungsdatum :

    1959


    Format / Umfang :

    17 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :