41–50 von 224 Ergebnissen
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    Chemical Reaction Effects on Heat Loads of CH4/O2 and H2/O2 Rockets

    Betti, Barbara | Online Contents | 2016
    Cooling of liquid rocket thrust chamber walls to allowable solid material temperatures induces near-wall chemical reactions, which are ...

    Coaxial Jet Flame Subject to Long-Wavelength Acoustic Oscillations

    Sirignano, William A | Online Contents | 2016
    -propellant rocket engine. Coaxial injection of fuel (outer flow) and oxygen (inner flow) is considered with chemical reaction in a thin flame and ...

    Combustion Heat-Release Effects on Supersonic Compressible Turbulent Boundary Layers

    Gao, Zhenxun | Online Contents | 2015
    Influences of heat release by the hydrogen combustion in supersonic turbulent boundary layers are numerically studied using Reynolds ...
    Schlagwörter: Chemical properties

    Combustion of Gelled Propellants Containing Microsized and Nanosized Aluminum Particles

    Negri, Michele | Online Contents | 2015
    probes. The chemical composition of the samples was determined, and the structure of the sampled combustion products was studied with microscopic ...

    Combustion of Synthetic Jet Fuel: Chemical Kinetic Modeling and Uncertainty Analysis

    Wagner, Andrew L | Online Contents | 2016

      Combustion of Synthetic Jet Fuel: Chemical Kinetic Modeling and Uncertainty Analysis

      Wagner, Andrew L | Online Contents | 2016
      Reaction mechanisms for jet-fuel combustion were built with the aim of providing a better description of the chemistry to reacting flow ...

    Compressible Model for Dilute Flows

    Petitpas, Fabien | Online Contents | 2015
    the case, for example, in solid rocket motors, where liquid droplets of aluminum at high temperature are ejected through a nozzle and endure ...

    Computational Fluid Dynamics Simulation of Hybrid Rockets of Different Scales

    Lazzarin, M | Online Contents | 2015
    work is the prosecution of a previous paper analyzing liquid injection in a lab-scale hybrid rocket. It is focused on the formulation of the ...

    Computational Fluid Dynamics Simulation of Tip-to-Tail for Hypersonic Test Vehicle

    Dharavath, Malsur | Online Contents | 2015
    for a flight Mach number of about six. Three-dimensional Navier-Stokes equations are solved along with the shear stress transport k-ω ...