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A Comparison Of Predicted And Measured Inlet Distortion Flows In A Subsonic Axial Inlet Flow Compressor Rotor
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Book Synopsis A Comparison of Predicted and Measured Inlet Distortion Flows in a Subsonic Axial Inlet Flow Compressor Rotor by : National Aeronautics and Space Adm Nasa
Download or read book A Comparison of Predicted and Measured Inlet Distortion Flows in a Subsonic Axial Inlet Flow Compressor Rotor written by National Aeronautics and Space Adm Nasa and published by . This book was released on 2020-04-09 with total page 200 pages. Available in PDF, EPUB and Kindle. Book excerpt: Detailed flow measurements were taken inside an isolated axial compressor rotor operating subsonically near peak efficiency. These Laser Anemometer measurements were made with two inlet velocity profiles. One profile consisted of an unmodified baseline flow, and the second profile was distorted by placing axisymmetric screens on the hub and shroud well upstream of the rotor. A detailed comparison in the rotor relative reference frame between a Navier-Stokes solver and the measured experimental results showed good agreement between the predicted and measured flows. A primary flow is defined in the rotor and deviations and the computed predictions is made to assess the development of a passage vortex due to the distortion of the inlet flow. Computer predictions indicate that a distorted inlet profile has a minimal effect on the development of the flow in the rotor passage and the resulting passage vortex. Owen, Albert K. Glenn Research Center AXIAL FLOW; FLOW DISTRIBUTION; FLOW VELOCITY; INLET FLOW; SUBSONIC FLOW; TURBOCOMPRESSORS; VELOCITY DISTRIBUTION; COMPRESSOR ROTORS; COMPUTATIONAL FLUID DYNAMICS; FLOW DISTORTION; LASER ANEMOMETERS; NAVIER-STOKES EQUATION; SHROUDS; VORTICES...
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781722892371 Total Pages :200 pages Book Rating :4.8/5 (923 download)
Book Synopsis A Comparison of Predicted and Measured Inlet Distortion Flows in a Subsonic Axial Inlet Flow Compressor Rotor by : National Aeronautics and Space Administration (NASA)
Download or read book A Comparison of Predicted and Measured Inlet Distortion Flows in a Subsonic Axial Inlet Flow Compressor Rotor written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-17 with total page 200 pages. Available in PDF, EPUB and Kindle. Book excerpt: Detailed flow measurements were taken inside an isolated axial compressor rotor operating subsonically near peak efficiency. These Laser Anemometer measurements were made with two inlet velocity profiles. One profile consisted of an unmodified baseline flow, and the second profile was distorted by placing axisymmetric screens on the hub and shroud well upstream of the rotor. A detailed comparison in the rotor relative reference frame between a Navier-Stokes solver and the measured experimental results showed good agreement between the predicted and measured flows. A primary flow is defined in the rotor and deviations and the computed predictions is made to assess the development of a passage vortex due to the distortion of the inlet flow. Computer predictions indicate that a distorted inlet profile has a minimal effect on the development of the flow in the rotor passage and the resulting passage vortex. Owen, Albert K. Glenn Research Center AXIAL FLOW; FLOW DISTRIBUTION; FLOW VELOCITY; INLET FLOW; SUBSONIC FLOW; TURBOCOMPRESSORS; VELOCITY DISTRIBUTION; COMPRESSOR ROTORS; COMPUTATIONAL FLUID DYNAMICS; FLOW DISTORTION; LASER ANEMOMETERS; NAVIER-STOKES EQUATION; SHROUDS; VORTICES...
Book Synopsis Scientific and Technical Aerospace Reports by :
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Book Synopsis 30th AIAA/ASME/SAE/ASEE Joint Propulsion Conference by :
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Book Synopsis Aeronautical Engineering: A Cumulative Index to a Continuing Bibliography (supplement 274) by :
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Book Synopsis Monthly Catalog of United States Government Publications by : United States. Superintendent of Documents
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Book Synopsis Monthly Catalog of United States Government Publications by :
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Book Synopsis Monthly Catalog of United States Government Publications, Cumulative Index by : United States. Superintendent of Documents
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Book Synopsis Aeronautical Engineering: A Cumulative Index to a Continuing Bibliography (supplement 287) by :
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Author :United States. National Aeronautics and Space Administration Scientific and Technical Information Division Publisher : ISBN 13 : Total Pages :966 pages Book Rating :4.F/5 ( download)
Book Synopsis NASA Scientific and Technical Reports by : United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Download or read book NASA Scientific and Technical Reports written by United States. National Aeronautics and Space Administration Scientific and Technical Information Division and published by . This book was released on 1970 with total page 966 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :United States. National Aeronautics and Space Administration. Scientific and Technical Information Division Publisher : ISBN 13 : Total Pages :962 pages Book Rating :4.E/5 ( download)
Book Synopsis A Selected Listing of NASA Scientific and Technical Reports by : United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Download or read book A Selected Listing of NASA Scientific and Technical Reports written by United States. National Aeronautics and Space Administration. Scientific and Technical Information Division and published by . This book was released on 1970 with total page 962 pages. Available in PDF, EPUB and Kindle. Book excerpt:
