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Showing 1 to 20 of 593 for “"compressor"”.

  1. Unsteady compressor distortion response and compressor instability

    Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1990.

    mit Repository record for Unsteady compressor distortion response and compressor instability (opens in a new tab)

  2. Rotary compressor model for investigating compressor performance and reliability

    Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 1998.

    mit Repository record for Rotary compressor model for investigating compressor performance and reliability (opens in a new tab)

  3. Axial compressor stall.

    … experimental investigation of rotating stall in compressors of high hub-tip ratio. Measurements were obtained in builds of one to four stages, covering a wide range of design flow rates and also a change in design reaction. The purpose of the experimental work has been to gain a better …

    cambridge Repository record for Axial compressor stall. (opens in a new tab)

  4. Centrifugal compressor aerodynamics

    cambridge

  5. Compressor leading edges

    Compressor blades often have a small 'spike' in the surface pressure distribution at the leading edge. This may result from blade erosion, manufacture defects or compromises made in the original design process. In this thesis it is shown that these spikes will increase the loss generated by a blade …

    cambridge Repository record for Compressor leading edges (opens in a new tab)

  6. Miniature HCCI Engine Compressor

    … A prototype miniature free-piston engine compressor runs for up to 30 s. New pistons and cylinder liners with coatings did not improve reliability when implemented in the engine. The engine stalled because pressure could not be held in the cylinder due to blow-by leakage caused by too …

    umn Repository record for Miniature HCCI Engine Compressor (opens in a new tab)

  7. Axial compressor stability enhancement

    … at all times. One source of instability is compressor stall. Stall problems can be reduced by machining cavities into the compressor casing adjacent to the rotor blades. This ‘casing treatment’ is the focus of the present work. Two treatment configurations are tested: circumferential grooves …

    cambridge Repository record for Axial compressor stability enhancement (opens in a new tab)

  8. High Speed Compressor Design

    Abstract: High Speed Compressor Design A long-standing paradox exists in high speed compressor blade design. As the inlet flow to a row of blades approaches the speed of sound, the two-dimensional (2D) design of that blade row becomes exceptionally difficult, with designers laboriously trying to …

    cambridge Repository record for High Speed Compressor Design (opens in a new tab)

  9. Axial compressor reversed flow performance

    Thesis (Ph.D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1985.

    mit Repository record for Axial compressor reversed flow performance (opens in a new tab)

  10. Modular Multi-Stage Axial Compressor Design

    … components, such as multi-stage axial compressors. It is the objective of this approach to utilize a "core" module in all the compressors, thus maximizing commonality and minimizing all relevant development, design, manufacture, procurement, and service costs; these reductions in cost …

    embry-riddle Repository record for Modular Multi-Stage Axial Compressor Design (opens in a new tab)

  11. OPTIMIZATION OF A PIEZOELECTRIC ACOUSTICAL COMPRESSOR

    A one-dimensional, axisymmetric, linear finite element model describing a fluid interacting with a piezoelectric actuator is developed. This system is used to generate finite amplitude standing waves in an acoustic cavity with rigid walls. The model includes the effects of viscous and thermal …

    maryland Repository record for OPTIMIZATION OF A PIEZOELECTRIC ACOUSTICAL COMPRESSOR (opens in a new tab)

  12. The Design of Aspirated Compressor Bleed

    Compressor bleed refers to the removal of flow from part way through the compressor for use in turbine cooling and other operational applications. Typical bleed systems in Industrial Gas Turbines comprise of an annular slot in the compressor casing, leading to external cavities. Aspiration refers …

    cambridge Repository record for The Design of Aspirated Compressor Bleed (opens in a new tab)

  13. Three-dimensional Mechanisms in Compressor Flows

    Three-dimensional design is central to all modern compressor design systems, but many of these methods still rely on a two-dimensional and sectional view of aerodynamics at their core. In this thesis it is argued that this view fundamentally limits design by not considering the effect, on …

    cambridge Repository record for Three-dimensional Mechanisms in Compressor Flows (opens in a new tab)

  14. Three dimensional design of compressor blades.

    cambridge

  15. Active control of centrifugal-compressor surge

    Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1989.

    mit Repository record for Active control of centrifugal-compressor surge (opens in a new tab)

  16. Modelling high speed multistage compressor stability

    Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1991.

    mit Repository record for Modelling high speed multistage compressor stability (opens in a new tab)

  17. Probabilistic aerothermal design of compressor airfoils

    … known in detail about its impact on aerothermal compressor performance. In this work, statistical and probabilistic techniques were used to assess the impact of geometric and operating condition uncertainty on axial compressor performance. High-fidelity models of geometric variability were …

    mit Repository record for Probabilistic aerothermal design of compressor airfoils (opens in a new tab)

  18. Flow losses in supersonic compressor cascades

    … mechanisms that affect the flow in supersonic compressor cascades have been reviewed, including the changes in shock geometry that will occur with back pressure for both started and unstarted operation. Compressible fluid mechanics has been applied to the known shock geometry to obtain a …

    vt Repository record for Flow losses in supersonic compressor cascades (opens in a new tab)

  19. Vibration Analysis of a Fan/Compressor Blade

    … of this thesis is the vibration analysis of compressor/fan blade using three-dimensional finite element analysis together with various analytical approaches. First, the analytical solutions were established using various analytical methods, Bernoulli-Euler, Rayleigh, Rayleigh-Ritz, …

    embry-riddle Repository record for Vibration Analysis of a Fan/Compressor Blade (opens in a new tab)

  20. Robust design methodologies: application to compressor blades

    Compressor blades are subtle aerodynamic shapes designed after years of research and insight. They inevitably show deviations from their desired shapes due to manufacturing errors, erosion or foreign object damage. In the present study we focus on seeking compressor blade geometries, that are …

    soton Repository record for Robust design methodologies: application to compressor blades (opens in a new tab)

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