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Showing 1 to 4 of 4 for “"Überschallstaustrahltriebwerk"”.

  1. Wärmebelastung der Brennkammer eines Staustrahltriebwerks mit Überschallverbrennung

    The aim of the dissertation project is the numerical simulation of the flow in a scramjet combustion chamber with diabatic walls. In order to analyze the aerothermal load on the structure and to determine the energy loss of the flow, an integrated fluid-thermal-structural analysis is performed. Of …

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  2. Numerical investigations of relaminarization in scramjet flows

    The numerical investigations of relaminarization using statistical turbulence models are presented. The goal is to identify suitable models that can be used in the design and development process of a 3D scramjet inlet by means of numerical methods. The computations were performed using a …

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  3. Experimentelle Untersuchungen zur Düsen- und Heckströmung eines Scramjets

    In the framework of the present thesis two different Single Expansion Ramp Nozzles (SERN) were experimentally investigated. For these experimental investigations existing measurement techniques (PSI, Pitot, Schlieren photograph) and additional measurement methods (Pressure Sensitive Paint, …

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  4. Experimentelle Untersuchung der Innenverdichtung eines Hyperschalltriebwerkeinlaufs mit Überschalldurchströmung

    The main topic of the research project is the experimental investigation of the inner compression of ramjet inlets with supersonic combustion (scramjet). The work focuses on the isolator section, located between the Inlet and the combustion chamber. The main Task of the isolator is he deceleration …

    aachen Repository record for Experimentelle Untersuchung der Innenverdichtung eines Hyperschalltriebwerkeinlaufs mit Überschalldurchströmung (opens in a new tab)