Performance Of A High Work Low Aspect Ratio Turbine Stator Tested With A Realistic Inlet Radial Temperature Gradient PDF Download
Are you looking for read ebook online? Search for your book and save it on your Kindle device, PC, phones or tablets. Download Performance Of A High Work Low Aspect Ratio Turbine Stator Tested With A Realistic Inlet Radial Temperature Gradient PDF full book. Access full book title Performance Of A High Work Low Aspect Ratio Turbine Stator Tested With A Realistic Inlet Radial Temperature Gradient.
Author | : National Aeronautics and Space Administration (NASA) |
Publisher | : Createspace Independent Publishing Platform |
Total Pages | : 32 |
Release | : 2018-07-09 |
Genre | : |
ISBN | : 9781722481445 |
Download Performance of a High-Work, Low-Aspect-Ratio Turbine Stator Tested with a Realistic Inlet Radial Temperature Gradient Book in PDF, ePub and Kindle
A 0.767-scale model of a turbine stator designed for the core of a high-bypass-ratio aircraft engine was tested with uniform inlet conditions and with an inlet radial temperature profile simulating engine conditions. The principal measurements were radial and circumferential surveys of stator-exit total temperature, total pressure, and flow angle. The stator-exit flow field was also computed by using a three-dimensional Navier-Stokes solver. Other than temperature, there were no apparent differences in performance due to the inlet conditions. The computed results compared quite well with the experimental results. Stabe, Roy G. and Schwab, John R. Glenn Research Center RTOP 505-62-3B...
Author | : |
Publisher | : |
Total Pages | : 34 |
Release | : 1991 |
Genre | : |
ISBN | : |
Download Performance of a High-work, Low-aspect-ratio Turbine Stator Tested with a Realistic Inlet Radial Temperature Gradient Book in PDF, ePub and Kindle
Author | : Roy G. Stabe |
Publisher | : |
Total Pages | : |
Release | : 1984 |
Genre | : Axial flow |
ISBN | : |
Download Performance of a High-work Low Aspect Ratio Turbine Tested with a Realistic Inlet Radial Temperature Profile Book in PDF, ePub and Kindle
Author | : |
Publisher | : |
Total Pages | : 1460 |
Release | : 1991 |
Genre | : Aeronautics |
ISBN | : |
Download Scientific and Technical Aerospace Reports Book in PDF, ePub and Kindle
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Author | : |
Publisher | : |
Total Pages | : 538 |
Release | : 1991 |
Genre | : Aeronautics |
ISBN | : |
Download Aeronautical Engineering Book in PDF, ePub and Kindle
Author | : |
Publisher | : |
Total Pages | : 1662 |
Release | : 1991 |
Genre | : Government reports announcements & index |
ISBN | : |
Download Government Reports Annual Index Book in PDF, ePub and Kindle
Author | : |
Publisher | : |
Total Pages | : 638 |
Release | : 1993 |
Genre | : Periodicals |
ISBN | : |
Download Publications in Engineering Book in PDF, ePub and Kindle
Author | : |
Publisher | : |
Total Pages | : 1112 |
Release | : |
Genre | : Government publications |
ISBN | : |
Download Monthly Catalog of United States Government Publications Book in PDF, ePub and Kindle
Author | : |
Publisher | : |
Total Pages | : 566 |
Release | : 1986 |
Genre | : Airplanes |
ISBN | : |
Download A Collection of Technical Papers Book in PDF, ePub and Kindle
Author | : Kenneth C. Hall |
Publisher | : Springer Science & Business Media |
Total Pages | : 648 |
Release | : 2006-03-08 |
Genre | : Technology & Engineering |
ISBN | : 9781402042676 |
Download Unsteady Aerodynamics, Aeroacoustics and Aeroelasticity of Turbomachines Book in PDF, ePub and Kindle
This textbook is a collection of technical papers that were presented at the 10th International Symposium on Unsteady Aerodynamics, Aeroacoustics, and Aeroelasticity of Turbomachines held September 8-11, 2003 at Duke University in Durham, North Carolina. The papers represent the latest in state of the art research in the areas of aeroacoustics, aerothermodynamics, computational methods, experimental testing related to flow instabilities, flutter, forced response, multistage, and rotor-stator effects for turbomachinery.