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  • 1
    Publication Date: 2019-06-28
    Description: Package of five computer programs is used to study trajectories of particles in radial-inflow turbines. Programs enable designer to predict areas of turbine that will be most affected by particle ingestion.
    Keywords: MECHANICS
    Type: LEW-12561 , NASA Tech Briefs (ISSN 0145-319X); 2; 3; P. 3
    Format: text
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  • 2
    Publication Date: 2019-06-27
    Description: The particle motion in two-dimensional free and forced inward flowing vortices is considered. A particle in such a flow field experiences a balance between the aerodynamic drag forces that tend to drive erosive particles toward the axis, and centrifugal forces that prevent these particles from traveling toward the axis. Results predict that certain sizes of particles will achieve a stable orbit about the turbine axis in the inward flowing free vortex. In this condition, the radial drag force is equal to the centrifugal force. The sizes of particles that will achieve a stable orbit is shown to be related to the gas flow velocity diagram at a particular radius. A second analysis yields a description of particle sizes that will experience a centrifugal force that is greater than the radial component of the aerodynamic drag force for a more general type of particle motion.
    Keywords: PROPULSION SYSTEMS
    Type: NASA-CR-134616
    Format: application/pdf
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  • 3
    Publication Date: 2019-06-27
    Description: Computer programs used to study the trajectories of particles in the radial inflow turbines are presented. The general technique of each program is described. A set of subroutines developed during the study are described. Descriptions, listings, and typical examples of each of the main programs are included.
    Keywords: AIRCRAFT PROPULSION AND POWER
    Type: NASA-CR-134787
    Format: application/pdf
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  • 4
    Publication Date: 2019-06-27
    Description: Similarity parameters from the equations of motion of particles immersed in a gas flow are derived. These parameters relate the particles which follow a certain trajectory in an equivalent cold gas turbine to particles that will follow the same trajectory in a real hot gas turbine. Numerical solutions of the trajectories that particles follow in the vortex and rotor regions of a radial inflow turbine are used to verify the range of Reynolds numbers in which the derived similarity parameters are applicable. In addition, an example is presented of typical particle sizes that can be observed in high speed photographic data collection and at the same time simulate the trajectories of particles in a real hot gas turbine.
    Keywords: PROPULSION SYSTEMS
    Type: NASA-CR-134589
    Format: application/pdf
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  • 5
    Publication Date: 2019-06-27
    Description: An analytic study of the rate at which material is removed by ingested dust impinging on the internal surfaces of a typical radial inflow turbine is presented. Results show that there are several regions which experience very severe erosion loss, and other regions that experience moderate levels of erosion loss: (1) the greatest amount of material loss occurs on the trailing edges of the nozzle blades where very high velocity, moderate angle impacts occur. The tip regions of ductile materials are also subjected to serious levels of erosion loss; (2) moderate amounts of erosion occur near the end of the scroll and on a few of the nozzle blades near this location. Results are presented in the form of surface contours that exist on the scroll and blade surfaces after continuous particulate ingestion with time.
    Keywords: MECHANICAL ENGINEERING
    Type: NASA-CR-134677
    Format: application/pdf
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  • 6
    Publication Date: 2019-06-27
    Description: The theoretical trajectories that erosive particles follow in the gas flow fields of a typical radial inflow turbine were investigated. A discussion of the theoretical trajectories that the particles follow in the scroll, in the nozzles, in the vortex between the nozzles and the rotor, and in the rotor passages is included. The results are presented in terms of the characteristic length, a similarity parameter which relates the particles that follow the same trajectory in equivalent flow fields. For Vol, 1, see N74-19395.
    Keywords: AIRCRAFT PROPULSION AND POWER
    Type: NASA-CR-134700
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  • 7
    Publication Date: 2019-07-13
    Keywords: AERODYNAMICS
    Type: ASME PAPER 74-GT-65 , Gas Turbine Conference and Products Show; Mar 30, 1974 - Apr 04, 1974; Zurich; Switzerland
    Format: text
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  • 8
    Publication Date: 2019-07-13
    Description: The results of analytical and experimental studies of the trajectories that atmospheric dust particles follow as they move through a radial inflow turbine are presented. The study reveals the nature of the impacts that occur within the turbine and indicates which surfaces are expected to experience the most severe erosion. In addition, a dimensionless parameter is derived which can be used during preliminary design analysis to indicate the sizes of the particles that will be most damaging to the turbine.
    Keywords: AERODYNAMICS
    Type: AIAA PAPER 75-844 , American Institute of Aeronautics and Astronautics, Fluid and Plasma Dynamics Conference; Jun 16, 1975 - Jun 18, 1975; Hartford, CT
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