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Exhaust Gas Pressure And Temperature Survey Of F404 Ge 400 Turbofan Engine
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Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781725981010 Total Pages :32 pages Book Rating :4.9/5 (81 download)
Book Synopsis Exhaust-Gas Pressure and Temperature Survey of F404-Ge-400 Turbofan Engine by : National Aeronautics and Space Administration (NASA)
Download or read book Exhaust-Gas Pressure and Temperature Survey of F404-Ge-400 Turbofan Engine written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-08-22 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt: An exhaust-gas pressure and temperature survey of the General Electric F404-GE-400 turbofan engine was conducted in the altitude test facility of the NASA Lewis Propulsion System Laboratory. Traversals by a survey rake were made across the exhaust-nozzle exit to measure the pitot pressure and total temperature. Tests were performed at Mach 0.87 and a 24,000-ft altitude and at Mach 0.30 and a 30,000-ft altitude with various power settings from intermediate to maximum afterburning. Data yielded smooth pressure and temperature profiles with maximum jet temperatures approximately 1.4 in. inside the nozzle edge and maximum jet temperatures from 1 to 3 in. inside the edge. A low-pressure region located exactly at engine center was noted. The maximum temperature encountered was 3800 R. Walton, James T. and Burcham, Frank W., Jr. Armstrong Flight Research Center NASA-TM-88273, H-1375, NAS 1.15:88273 RTOP 533-02-08...
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