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Showing 1 to 20 of 814 for “"Flow field"”.

  1. Development of nonintrusive flow field imaging diagnostics

    Includes bibliographical references.

    colo-mines Repository record for Development of nonintrusive flow field imaging diagnostics (opens in a new tab)

  2. Flow-field structure in wide-angled diffusers

    Includes bibliographical references (leaves 121-131).

    cape-town Repository record for Flow-field structure in wide-angled diffusers (opens in a new tab)

  3. A secondary flow approach to the inlet vortex flow field

    … (or ground vortex) phenomenon. The vorticity field associated with the vortex is investigated using a secondary flow approach. In this approach the flow is assumed to be composed of an irrotational primary flow and a weak shear flow, with the vortex filaments associated with the latter being …

    mit Repository record for A secondary flow approach to the inlet vortex flow field (opens in a new tab)

  4. Flow field modifications and wave development in a plane Poiseuille flow

    Thesis (Sc. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1991.

    mit Repository record for Flow field modifications and wave development in a plane Poiseuille flow (opens in a new tab)

  5. Multi-Property Internal Flow Field Quantification using Molecular Filtered Rayleigh Scattering

    … the multi-property quantification of internal flow fields. Validation is challenging in applying computational fluid dynamics (CFD) solutions to real-world scenarios, necessitating benchmark measurements with well-defined uncertainties. The ideal instrument for achieving the required …

    vt Repository record for Multi-Property Internal Flow Field Quantification using Molecular Filtered Rayleigh Scattering (opens in a new tab)

  6. Experimental investigation of the flow field in a missile launch tube

    An investigation of the flow field during eject of a cruise missile from the launch tube was undertaken using a "cold" flow simulation. A facility was developed whereby various design changes in the missile ejection apparatus, denoted the vertical support assembly, could be quickly and easily …

    vt Repository record for Experimental investigation of the flow field in a missile launch tube (opens in a new tab)

  7. Supersonic flow field visualization studies of the MÅ = 6 price waverider planform

    Supersonic tests of the conical flow derived MÅ Ê» = 6 (design) Price waverider planform were conducted using the Naval Postgraduate School wind tunnel. These tests are part of a continuing effort to study the characteristics of waverider configured vehicles. Two sting-mounted, flat-plate …

    nps Repository record for Supersonic flow field visualization studies of the MÅ = 6 price waverider planform (opens in a new tab)

  8. Doppler global velocimetry measurements in a wing flow field with tip blowing

    A two-component Doppler global velocimetry (DGV) system has been developed, improved, and tested. DGV is a non-intrusive optical velocity measurement technique. DGV measures the Doppler shift of the frequency of the light scattered by seed particles at a specific location. The velocity of the …

    wvu Repository record for Doppler global velocimetry measurements in a wing flow field with tip blowing (opens in a new tab)

  9. Experimental investigation of the flow field during combustion in narrow circular ducts

    … was studied with the intent of determining the flow structure that underlay the observed oscillatory motion. The fluid motion during the oscillations was visualized by seeding TiO2 micron-sized particles. Particle Streak Velocimetry was used to obtain flow-field measurements during the …

    uiuc Repository record for Experimental investigation of the flow field during combustion in narrow circular ducts (opens in a new tab)

  10. Post-stall hysteresis and flow field unsteadiness on an NACA 0012 airfoil

    The current study was conducted to understand flow field unsteadiness associated with static stall hysteresis on an NACA 0012 airfoil at Rec = 1.0 × 10^6. Unsteady pressure measurements were acquired to evaluate the performance of the airfoil, and a hysteresis loop was identified in the vicinity of …

    uiuc Repository record for Post-stall hysteresis and flow field unsteadiness on an NACA 0012 airfoil (opens in a new tab)

  11. A new method for calculating the flow field in a dump combustor

    An elliptic/parabolic procedure for solving the flow field in a dump combustor is described. The elliptic calculation is used at the dump combustor entrance and a parabolic calculation downstream. The calculations are restricted to steady axisymmetric nonreactive incompressible flow. A great …

    vt Repository record for A new method for calculating the flow field in a dump combustor (opens in a new tab)

  12. Flow Field Computations of Combustor-Turbine Interactions in a Gas Turbine Engine

    … between the combustor and turbine. The flow field at a combustor exit shows non-uniformities in pressure, temperature, and velocity in the pitch and radial directions. This inlet profile to the turbine can have a considerable effect on the development of the secondary flows through the …

    vt Repository record for Flow Field Computations of Combustor-Turbine Interactions in a Gas Turbine Engine (opens in a new tab)

  13. Flow Field and Soot Formation Characteristics in Swirl-stabilized Non-premixed Turbulent Flames

    Soot formation and evolution in relation with the flow fields were investigated experimentally in turbulent swirl-stabilized non-premixed flames using three different fuels: methane, ethanol and aviation Jet A-1. The studied flames were confined and stabilized in a model gas turbine combustor with …

    toronto-retro Repository record for Flow Field and Soot Formation Characteristics in Swirl-stabilized Non-premixed Turbulent Flames (opens in a new tab)

  14. 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)

  15. Effect of Heat Transfer on Flow Field at Low Reynolds Numbers in Verticaltubes

    Made available in DSpace on 2014-12-05T17:15:30Z (GMT). No. of bitstreams: 1 6000230.pdf: 8147700 bytes, checksum: 7c04c8e1ee39e0ce32c266eac3d9694f (MD5) Previous issue date: 1959

    uiuc Repository record for Effect of Heat Transfer on Flow Field at Low Reynolds Numbers in Verticaltubes (opens in a new tab)

  16. Characterization of the flow field response to vaneless space reduction in centrifugal compressors

    The unsteady three-dimensional flow field for two centrifugal compressors of nearly identical design (one with a marginally smaller impeller-diffuser gap) is interrogated to assess the difference in the time averaged performance and unsteady loading characteristics of the impeller blades. …

    mit Repository record for Characterization of the flow field response to vaneless space reduction in centrifugal compressors (opens in a new tab)

  17. Flow/field model of a hot magnetized plasma interacting with a cold neutral atmosphere

    … that possess neither an intrinsic magnetic field nor a significant ionosphere have not been well studied. We have constructed a model to simulate the interaction between a hot magnetized plasma and a planet containing only a neutral atmosphere. Examination of the boundary conditions that …

    rice Repository record for Flow/field model of a hot magnetized plasma interacting with a cold neutral atmosphere (opens in a new tab)

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