Global ETD Search

Search theses and dissertations gathered from participating repositories worldwide. Every result links back to the library that holds it. No account is needed.

Results

Showing 1 to 20 of 26 for “"Base Pressure"”.

  1. Base Pressure Problems Associated With Supersonic Axisymmetric External Flow Configurations

    Made available in DSpace on 2014-12-13T19:55:23Z (GMT). No. of bitstreams: 1 7524433.pdf: 3022190 bytes, checksum: 87de53c9eb27a879ba0a26697cc54f5d (MD5) Previous issue date: 1975

    uiuc Repository record for Base Pressure Problems Associated With Supersonic Axisymmetric External Flow Configurations (opens in a new tab)

  2. Analytical and Experimental Study of the Axially-Symmetric Supersonic Base Pressure Problem

    Made available in DSpace on 2014-12-05T19:15:56Z (GMT). No. of bitstreams: 1 5904589.pdf: 4526857 bytes, checksum: ea67dc586d3f5a675540d838bb26c5c8 (MD5) Previous issue date: 1959

    uiuc Repository record for Analytical and Experimental Study of the Axially-Symmetric Supersonic Base Pressure Problem (opens in a new tab)

  3. Base Pressure Problems Associated With an Axisymmetric Transonic Flow Past a Backward Facing Step

    Made available in DSpace on 2014-12-13T19:55:27Z (GMT). No. of bitstreams: 1 7804072.pdf: 3116092 bytes, checksum: c4888928ad717df358d1660e293794c7 (MD5) Previous issue date: 1977

    uiuc Repository record for Base Pressure Problems Associated With an Axisymmetric Transonic Flow Past a Backward Facing Step (opens in a new tab)

  4. An experimental determination of the trailing-edge base pressure on blades in transonic turbine cascades

    … documents an experimental investigation of the base (trailing edge) pressure and its approximate distribution on a transonic turbine blade. Since the base pressure plays an important role in determining the profile loss on blades with thick trailing edges, both the base pressure and the blade …

    vt Repository record for An experimental determination of the trailing-edge base pressure on blades in transonic turbine cascades (opens in a new tab)

  5. The Influence of Finite Bleed Velocities on The Effectiveness of Base Bleed in The Two-Dimensional Supersonic Base Pressure Problem

    Made available in DSpace on 2014-12-05T19:15:54Z (GMT). No. of bitstreams: 1 0020898.pdf: 2450533 bytes, checksum: 9229436e35d4ba0a65ae00cc108838fa (MD5) Previous issue date: 1957

    uiuc Repository record for The Influence of Finite Bleed Velocities on The Effectiveness of Base Bleed in The Two-Dimensional Supersonic Base Pressure Problem (opens in a new tab)

  6. A Study of the Base Pressure Problem for Supersonic Two-Dimensional Flow in Which the Approaching Stream Has Transient Properties

    Made available in DSpace on 2014-12-05T19:15:58Z (GMT). No. of bitstreams: 1 6104317.pdf: 1769323 bytes, checksum: 1ca32c6324f3b5d590e44e013047b6d5 (MD5) Previous issue date: 1961

    uiuc Repository record for A Study of the Base Pressure Problem for Supersonic Two-Dimensional Flow in Which the Approaching Stream Has Transient Properties (opens in a new tab)

  7. The Non-Isoenergetic Turbulent Jet Mixing of a Two-Dimensional Supersonicjet With Consideration of Its Influence on The Base Pressure Problem

    Made available in DSpace on 2014-12-05T19:15:51Z (GMT). No. of bitstreams: 1 0013542.pdf: 2446937 bytes, checksum: 1ad23c458f116f75349fc30ffd504036 (MD5) Previous issue date: 1955

    uiuc Repository record for The Non-Isoenergetic Turbulent Jet Mixing of a Two-Dimensional Supersonicjet With Consideration of Its Influence on The Base Pressure Problem (opens in a new tab)

  8. Ram-jet combustion based on shock/flame interaction

    … of shock/wake and shock/flame interaction on the base pressure of axisymmetric bodies at Mach 2 has been carried out. This investigation has determined the effects of various forms of shock generator (axisymmetric cowls, twodimensional wedges and 'delta' wings) on the base pressure. Shock waves …

    cranfield Repository record for Ram-jet combustion based on shock/flame interaction (opens in a new tab)

  9. Active control of massively separated high-speed/base flows with electric arc plasma actuators

    … multiple electric-arc plasma discharges near the base corner separation point. The control authority of electric arc plasma actuators on a supersonic axisymmetric base flow was evaluated for several actuator geometries, frequencies, forcing modes, duty cycles/on-times, and currents. Initially, an …

    uiuc Repository record for Active control of massively separated high-speed/base flows with electric arc plasma actuators (opens in a new tab)

  10. Control of supersonic axisymmetric base flows using passive splitter plates and pulsed plasma actuators

    … control on the near-wake downstream of a blunt-based axisymmetric body in supersonic flow has been conducted. To better understand and control the physical phenomena that govern these massively separated high-speed flows, this research examined both passive and active flow-control methodologies …

    uiuc Repository record for Control of supersonic axisymmetric base flows using passive splitter plates and pulsed plasma actuators (opens in a new tab)

  11. Effect of Adaptive Tabs on Drag of a Square-Base Bluff Body

    … wind tunnel testing of a 0.127m by 0.127m square-base bluff body to test the effectiveness of trailing edge tabulations to reduce drag in the Cal Poly 0.912m by 1.219 m low-speed wind tunnel. To accomplish this, the boundary layer was first measured on the trailing edge of the model for the three …

    calpoly Repository record for Effect of Adaptive Tabs on Drag of a Square-Base Bluff Body (opens in a new tab)

  12. Wake closure conditions in plug nozzle flowfields

    … of the flow determines the dependence of the base pressure on the ambient environment, and therefore affects overall thrust. An experimental, numerical, and analytical investigation characterized the transition of the wake between closed and numerical, and analytical investigation …

    washington Repository record for Wake closure conditions in plug nozzle flowfields (opens in a new tab)

  13. Projectile thrust-drag optimization with external burning

    External burning increases base pressure. The characteristic and linearized equations with heat addition are discuss ed, and the condition for maintaining irrotationa ity with heat addition is derived. A transition model, which extends the Crocco-Lees base flow model, and a spin model are …

    nps Repository record for Projectile thrust-drag optimization with external burning (opens in a new tab)

  14. Modification of an ultra-high-vacuum scanning tunneling microscope for silicon nanostructure fabrication

    … hours to 3 hours. The capillary doser lowers the base pressure during the silicon growth experiment by two orders of magnitude. The system operation after the system modification was tested. The system is now ready for subsequent silicon nanostructure growth using disilane gas.

    uiuc Repository record for Modification of an ultra-high-vacuum scanning tunneling microscope for silicon nanostructure fabrication (opens in a new tab)

  15. The drag and lift characteristics of a cylinder placed near a plane surface

    Surface pressure, drag and lift coefficients have been experimentally determined for a right circular cylinder located near a plane surface and placed in a cross flow of air. Parametric studies were carried out for Reynolds numbers varying from 90,000 to 250,000, three plate lengths and a variety …

    nps Repository record for The drag and lift characteristics of a cylinder placed near a plane surface (opens in a new tab)

  16. Measurements and Visualizations of a Three-Dimensional Compressible Base Flow

    … varying strength at the angular discontinuity, a base-edge expansion fan, a separated shear layer, an asymmetric recirculation region, and a turbulent wake. A strong secondary circumferential flow, which develops along the afterbody due to pressure gradients on its surface, results in the …

    uiuc Repository record for Measurements and Visualizations of a Three-Dimensional Compressible Base Flow (opens in a new tab)

  17. A study of micromachined displacement pumps for vacuum generation

    … and analyzers are normally operated at the pressure range lower than a few millitorr. We are developing a micromachined vacuum pump that is comprised of a mechanical rough pump integrated with micromachined ion-pumps. The rough pump generates a low vacuum of tens of torr from atmospheric …

    mit Repository record for A study of micromachined displacement pumps for vacuum generation (opens in a new tab)

  18. Design of curved electrodes to enable large stroke -- low voltage micro actuators

    … practical devices. The first method uses air pressure to plastically deform a silicon membrane at high temperature. During wafer bonding, gas is trapped behind a thin silicon membrane. High temperature annealing causes the gas to pressurize, plastically deforming the silicon membrane. A model …

    mit Repository record for Design of curved electrodes to enable large stroke -- low voltage micro actuators (opens in a new tab)

Page 1 of 2