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Showing 1 to 7 of 7 for “"Normal Injection"”.

  1. Combined tangential-normal injection into a supersonic flow

    A combination of tangential and normal air injection into a Mach 3 airflow was experimentally studied. A rearward facing slot producing tangential injection at a nominal Mach number 1.7 was operated at several different total pressures. An array of transverse tubes of height equal to the slot …

    vt Repository record for Combined tangential-normal injection into a supersonic flow (opens in a new tab)

  2. A study of the normal injection of hydrogen into a heated supersonic flow using planar laser-induced fluoresence

    Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1992.

    mit Repository record for A study of the normal injection of hydrogen into a heated supersonic flow using planar laser-induced fluoresence (opens in a new tab)

  3. Injection of liquid fuels in supersonic airstreams

    … range 1500 to 2300ºF, injectant flow rate and injection angles from 90º to 45º upstream. The experimental observations were: temperature measurements on the wall near the injector and in the flow downstream of injection self-luminosity photographs and infrared photographs taken with a …

    vt Repository record for Injection of liquid fuels in supersonic airstreams (opens in a new tab)

  4. The effect of flow structure on the combustion and heat transfer in a scramjet combustor

    … demonstrated combustor performance with parallel injection comparable to that reported using normal injection. This unusually rapid parallel jet mixing and combustion was obtained using swept ramp injectors with near-parallel injection. The experiments and calculations showed that the injectors …

    vt Repository record for The effect of flow structure on the combustion and heat transfer in a scramjet combustor (opens in a new tab)

  5. Numerical Studies of the Jet Interaction Flowfield with a Main Jet and an Array of Smaller Jets

    … interaction flowfield associated with the sonic injection of a gas into a high-speed crossflow was simulated by numerically solving the Reynolds Averaged Navier Stokes (RANS) equations. Turbulence was modeled through a first-order model, the Wilcox's 1988 k-w turbulence model. The computations …

    vt Repository record for Numerical Studies of the Jet Interaction Flowfield with a Main Jet and an Array of Smaller Jets (opens in a new tab)

  6. A mach 1.95 free-jet facility for experimental investigation of injectant flow patterns

    … techniques were evaluated in the facility. Normal, sonic injection of helium through a circular injector was studied as a way to evaluate nanoshadowgraph photography, oil flow photography, and infrared imaging as qualitative flow visualization methods. Quantitative measurements of the local …

    vt Repository record for A mach 1.95 free-jet facility for experimental investigation of injectant flow patterns (opens in a new tab)

  7. Innovative Transverse Jet Interaction Arrangements in Supersonic Crossflow

    … of low pressure typically found downstream of a normal, sonic injector in supersonic flow and also possibly increase in intensity of the upstream high-pressure region. The secondary jet would, in theory, "push" the primary jet further into the flow, increasing the size of the obstacle as seen by …

    vt Repository record for Innovative Transverse Jet Interaction Arrangements in Supersonic Crossflow (opens in a new tab)