A series of reports are presented on SCRAMjet studies, shock tunnel studies, and expansion tube studies. The SCRAMjet studies include: (1) Investigation of a Supersonic Combustion Layer; (2) Wall Injected SCRAMjet Experiments; (3) Supersonic Combustion with Transvers, Circular, Wall Jets; (4) Dissociated Test Gas Effects on SCRAMjet Combustors; (5) Use of Silane as a Fuel Additive for Hypersonic Thrust Production, (6) Pressure-length Correlations in Supersonic Combustion; (7) Hot Hydrogen Injection Technique for Shock Tunnels; (8) Heat Release - Wave Interaction Phenomena in Hypersonic Flows; (9) A Study of the Wave Drag in Hypersonic SCRAMjets; (10) Parametric Study of Thrust Production in the Two Dimensional SCRAMjet; (11) The Design of a Mass Spectrometer for use in Hypersonic Impulse Facilities; and (12) Development of a Skin Friction Gauge for use in an Impulse Facility. The shock tunnel studies include: (1) Hypervelocity flow in Axisymmetric Nozzles; (2) Shock Tunnel Development; and (3) Real Gas Efects in Hypervelocity Flows over an Inclined Cone. The expansion tube studies include: (1) Investigation of Flow Characteristics in TQ Expansion Tube; and (2) Disturbances in the Driver Gas of a Shock Tube.


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    Titel :

    Shock tunnel studies of scramjet phenomena, supplement 5


    Beteiligte:
    Casey, R. (Autor:in) / Stalker, R. J. (Autor:in) / Brescianini, C. P. (Autor:in) / Morgan, R. G. (Autor:in) / Jacobs, P. A. (Autor:in) / Wendt, M. (Autor:in) / Ward, N. R. (Autor:in) / Akman, N. (Autor:in) / Allen, G. A. (Autor:in) / Skinner, K. (Autor:in)

    Erscheinungsdatum :

    1990-10-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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    Shock tunnel studies of scramjet phenomena, supplement 6

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    Shock tunnel studies of scramjet phenomena, supplement 8

    Stalker, R. J. / Hollis, P. / Allen, G. A. et al. | NTRS | 1993