1–20 of 159 hits
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    WALL PRESSURE EFFECTS AND SHOCK-BOUNDARY LAYER INTERACTIONS IN A TRANSPIRATION COOLED SCRAMJET MODEL COMBUSTOR

    Strauss, Friedolin T. / Cragg, Stephan General. Patrick A. / Schlechtriem, Stefan | TIBKAT | 2020

    Understanding the Total Pressure Losses Nature in a Scramjet Combustor

    Palateerdham, Sasi Kiran / Peri, Lakshmi Narayana Phaneendra / Ingenito, Antonella et al. | TIBKAT | 2023

    Transient Heat Transfer in a Scramjet Forebody Under Varying Hypersonic Flow

    Kirupakaran, Gopinath Nagarajan / Govindarajan, K. V. / Mahapatra, Debiprosad Roy | TIBKAT | 2023

    TOWARDS MODELLING OF THERMAL PROTECTION SYSTEMS WITH TRANSPIRATION COOLING

    Bukva, Alexander / Christopher, Nicholas / Hickey, Jean-Pierre | TIBKAT | 2020

    TOWARDS A THRESHOLD-FREE DETECTION OF THE BOUNDARY LAYER EDGE AROUND A SUPERSONIC BLUNT-BODY

    Morilhat, Sylvain / Olazabal-Loumé, Marina / Bridel-Berthomeu, Thibault | TIBKAT | 2020

    The NASA-sponsored Maryland center for hypersonic education and research

    Lewis, Mark J. / Gupta, Ashwani K. | NTRS | 1995
    The Office of Aeronautics of the National Aeronautics and Space Administration has established a program to support university programs in ...
    Publisher: NASA National Aeronautics and Space Administration
    Keywords: Research And Support Facilities (Air)

    System Overview of the STAJe- 1 Payload

    Kunze, Jens / Paull, Allan | TIBKAT | 2023

    Supersonic Mixing Characteristics of an Internal Cross-Flow Effervescent Ramp Injector

    Dharan, Saran S. / Vaidyanathan, Aravind / Sln, Desikan | TIBKAT | 2023

    Supersonic Combustion Supported by Flameholders

    Vialta, Leda M. / Matos, Pedro A. / Barreta, Luiz G. et al. | TIBKAT | 2023