Use of sled system is recommended as methd of obtaining aerodynamic data in regime of high Mach and Reynolds numbers; description of sled designs and data collection system which is used successfully to acquire pressure data on cone-cylinders; data are compared with data from free-flight rockets, wind-tunnel tests and computer calculations; sled-testing appears promising method of simulating flight conditions at low altitudes at Mach numbers up to M equal 8; principal advantage is high degree of accuracy possible in determining actual test conditions, which include Mach number, static pressure, and static temperature; sleds may be used to collect other experimental data such as heat-transfer and boundary-layer transition. (17694)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    High-speed monorail rocket sleds for aerodynamic testing at high Reynolds numbers


    Weitere Titelangaben:

    J Spacecraft Rockets


    Beteiligte:
    Rigali, D.J. (Autor:in) / Feltz, L.V. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1968


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :