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Showing 1 to 14 of 14 for “"Mass Flow Ratio"”.

  1. A numerical investigation of s-duct flows with boundary-layer ingestion

    … conducted to further NASA's study of active flow control systems for a flush­-mounted inlet with significant boundary-­layer ingestion (BLI). In conjunction with a NASA-­sponsored research grant, the aim is to further accumulate knowledge and insight on the effectiveness of flow control …

    utc Repository record for A numerical investigation of s-duct flows with boundary-layer ingestion (opens in a new tab)

  2. Design and optimization of a humidifier for an HDH system

    … is a water treatment technology with low operational requirements that make it ideal for operation in the developing world. Researchers in the lab have just developed a novel design methodology for optimizing the performance of an HDH system based on thermal balancing, similar to the …

    mit Repository record for Design and optimization of a humidifier for an HDH system (opens in a new tab)

  3. Precipitation of micro/nanoparticles in enhanced high energy dissipation mixing systems

    Crystallization is the most common unit operation used in the pharmaceutical industry to synthesize active ingredients. Rapid development of a drug candidate is dependent on the ability to produce a desired drug substance with consistent properties, These properties include stability and purity, …

    njit Repository record for Precipitation of micro/nanoparticles in enhanced high energy dissipation mixing systems (opens in a new tab)

  4. Aerodynamic performance measurements of a fully scaled, film-coated, turbine stage

    The MIT Blowdown Turbine short duration test facility was used to experimentally measure the aerodynamic performance of a film-cooled turbine stage. Turbine torque, speed, mass flow, temperature, and pressure were measured and used to calculate efficiency. Pressure ratio, corrected speed, and …

    mit Repository record for Aerodynamic performance measurements of a fully scaled, film-coated, turbine stage (opens in a new tab)

  5. Aerodynamic performance of a transonic turbine blade passage in presence of upstream slot and mateface gap with endwall contouring

    … no studies exist in literature for transonic flow conditions. Experiments were performed at the Virginia Tech's linear, transonic blow down cascade facility. Measurements were carried out at design conditions (isentropic exit Mach number of 0.87, design incidence) without and with coolant …

    vt Repository record for Aerodynamic performance of a transonic turbine blade passage in presence of upstream slot and mateface gap with endwall contouring (opens in a new tab)

  6. Aerodynamics of Endwall Contouring with Discrete Holes and an Upstream Purge Slot Under Transonic Conditions with and without Blowing

    … aerodynamic performance by reducing secondary flow strength. The effects of endwall contouring with discrete holes and an upstream purge slot for a high turning (127") airfoil passage under transonic conditions are investigated. The total pressure loss and secondary flow field were measured for …

    vt Repository record for Aerodynamics of Endwall Contouring with Discrete Holes and an Upstream Purge Slot Under Transonic Conditions with and without Blowing (opens in a new tab)

  7. Numerical Examination of Flow Field Characteristics and Fabri Choking of 2D Supersonic Ejectors

    … Fabri choke and Fabri block aerodynamic flow patterns. The effect of primary to secondary stagnation pressure ratio on the efficiency of the ejector operation is measured using the entrainment ratio which is the secondary to primary mass flow ratio. The primary flow of the ejector is …

    calpoly Repository record for Numerical Examination of Flow Field Characteristics and Fabri Choking of 2D Supersonic Ejectors (opens in a new tab)

  8. Numerical simulation and modelling of the effect of film cooling on entropy noise in a stator blade row

    … fundamental understanding of how film cooling flows interact with entropy waves, and their influence on entropy noise generation. A 2D numerical framework has been developed for preliminary understanding of the problem, and then analysis of the effect of film cooling on the entropy noise …

    qu-belfast Repository record for Numerical simulation and modelling of the effect of film cooling on entropy noise in a stator blade row (opens in a new tab)

  9. Trailing Edge Aerodynamics: Flow Regimes, Geometry and Loss

    The flow at the trailing edge of a turbine blade at transonic air velocities can be extremely complex. Solid trailing edges can shed vortices in a manner known as transonic vortex shedding, where vortices form very close to the trailing edge and cause large trailing edge shear layer deflection. …

    cambridge Repository record for Trailing Edge Aerodynamics: Flow Regimes, Geometry and Loss (opens in a new tab)

  10. Heat Transfer Performance Improvement Technologies for Hot Gas Path Components in Gas Turbines

    … in order to ensure safe and durable operation, the hot gas path components are additionally supplemented with thermal barrier coatings (TBCs) and sophisticated cooling techniques. The present study focusses on two aspects of gas turbine cooling, namely augmented internal cooling and …

    vt Repository record for Heat Transfer Performance Improvement Technologies for Hot Gas Path Components in Gas Turbines (opens in a new tab)

  11. The effects of micro-vortex generators on normal shock wave/boundary layer interactions

    … interactions (SWBLIs) are complex flow phenomena that are important in the design and performance of internal supersonic and transonic flow fields such as engine inlets. This investigation was undertaken to study the effects of passive flow control devices on normal shock …

    uiuc Repository record for The effects of micro-vortex generators on normal shock wave/boundary layer interactions (opens in a new tab)

  12. Thermodynamic Analysis and Optimization of Supercritical Carbon Dioxide Brayton Cycles

    The power generation industry is facing new challenging issues regarding accelerating growth of electricity demand, fuel cost and environmental pollution. These challenges accompanied by concerns of energy resources becoming scarce necessitate searching for sustainable and economically competitive …

    ucf

  13. Numerical and experimental investigation of VG flow control for a low-boom inlet

    … (VGs) for shock/boundary layer interaction flow control in a novel external compression, axisymmetric, low-boom concept inlet was studied using numerical and experimental methods. The low-boom inlet design features a zero-angle cowl and relaxed isentropic compression centerbody spike, …

    uiuc Repository record for Numerical and experimental investigation of VG flow control for a low-boom inlet (opens in a new tab)

  14. Heat Transfer and Film Cooling Performance on a Transonic Converging Nozzle Guide Vane Endwall With Purge Jet Cooling and Dual Cavity Slashface Leakage

    … of implementing a dual cavity slashface configuration and varying slashface coolant leakage mass flow rate on the thermal performance for a 1st stage nozzle guide vane axisymmetric converging endwall. An upstream doublet staggered cylindrical hole jet cooling scheme provides additional purged …

    vt Repository record for Heat Transfer and Film Cooling Performance on a Transonic Converging Nozzle Guide Vane Endwall With Purge Jet Cooling and Dual Cavity Slashface Leakage (opens in a new tab)