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Laser Anemometer Measurements And Computations In An Annular Cascade Of High Turning Core Turbine Vanes
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Book Synopsis Laser Anemometer Measurements and Computations in an Annular Cascade of High Turning Core Turbine Vanes by : Louis J. Goldman
Download or read book Laser Anemometer Measurements and Computations in an Annular Cascade of High Turning Core Turbine Vanes written by Louis J. Goldman and published by . This book was released on 1992 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781722334598 Total Pages :38 pages Book Rating :4.3/5 (345 download)
Book Synopsis Laser Anemometer Measurements and Computations in an Annular Cascade of High Turning Core Turbine Vanes by : National Aeronautics and Space Administration (NASA)
Download or read book Laser Anemometer Measurements and Computations in an Annular Cascade of High Turning Core Turbine Vanes written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-05 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt: An advanced laser anemometer (LA) was used to measure the axial and tangential velocity components in an annular cascade of turbine stator vanes designed for a high bypass ratio engine. These vanes were based on a redesign of the first-stage stator, of a two-stage turbine, that produced 75 degrees of flow turning. Tests were conducted on a 0.771 scale model of the engine size stator. The advanced LA fringe system was designed to employ thinner than usual laser beams resulting in a 50-micron-diameter probe volume. Window correction optics were used to ensure that the laser beams did not uncross in passing through the curved optical access port. Experimental LA measurements of velocity and turbulence were obtained both upstream, within, and downstream of the stator vane row at the design exit critical velocity ratio of 0.896 at the hub. Static pressures were also measured on the vane surface. The measurements are compared, where possible with calculations from a 3-D inviscid flow analysis. The data are presented in both graphic and tabulated form so that they may be readily used to compare against other turbomachinery computations. Goldman, Louis J. and Seasholtz, Richard G. Glenn Research Center RTOP 505-62-52...
Book Synopsis Laser Anemometer Measurements and Computations for Transonic Flow Conditions in an Annular Cascade of High Turning Core Turbine Vanes by : National Aeronautics and Space Adm Nasa
Download or read book Laser Anemometer Measurements and Computations for Transonic Flow Conditions in an Annular Cascade of High Turning Core Turbine Vanes written by National Aeronautics and Space Adm Nasa and published by . This book was released on 2018-10-20 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: An advanced laser anemometer (LA) was used to measure the axial and tangential velocity components in an annular cascade of turbine stator vanes operating at transonic flow conditions. The vanes tested were based on a previous redesign of the first-stage stator in a two-stage turbine for a high-bypass-ratio engine. The vanes produced 75 deg of flow turning. Tests were conducted on a 0.771-scale model of the engine-sized stator. The advanced LA fringe system employed an extremely small 50-micron diameter probe volume. Window correction optics were used to ensure that the laser beams did not uncross in passing through the curved optical access port. Experimental LA measurements of velocity and turbulence were obtained at the mean radius upstream of, within, and downstream of the stator vane row at an exit critical velocity ratio of 1.050 at the hub. Static pressures were also measured on the vane surface. The measurements are compared, where possible, with calculations from a three-dimensional inviscid flow analysis. Comparisons were also made with the results obtained previously when these same vanes were tested at the design exit critical velocity ratio of 0.896 at the hub. The data are presented in both graphical and tabulated form so that they can be readily compared against other turbomachinery computations. Goldman, Louis J. Glenn Research Center RTOP 505-62-52...
Book Synopsis Laser Anemometer Measurements and Computations for Transonic Flow Conditions in an Annular Cascade of High Turning Core Turbine Vanes by : Louis J. Goldman
Download or read book Laser Anemometer Measurements and Computations for Transonic Flow Conditions in an Annular Cascade of High Turning Core Turbine Vanes written by Louis J. Goldman and published by . This book was released on 1993 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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