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Thrust Induced Effects On Low Speed Aerodynamics Of Fighter Aircraft Langley 4 By 7 Meter Tunnel
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Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781724750679 Total Pages :28 pages Book Rating :4.7/5 (56 download)
Book Synopsis Thrust-Induced Effects on Low-Speed Aerodynamics of Fighter Aircraft. [Langley 4- By 7-Meter Tunnel] by : National Aeronautics and Space Administration (NASA)
Download or read book Thrust-Induced Effects on Low-Speed Aerodynamics of Fighter Aircraft. [Langley 4- By 7-Meter Tunnel] written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-08-06 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: Results of NASA Langley has conducted wind-tunnel investigations of several fighter configurations conducted to determine the effects of both thrust vectoring and spanwise blowing are reviewed. A recent joint NASA/Grumman Aerospace Corporation/U.S. Air Force Wright Aeronautical Laboratory wind-tunnel investigation was conducted to examine the effects of spanwise blowing on the trailing-edge flap system. This application contrasts with the more familiar method of spanwise blowing near the wing leading edge. Another joint program among NASA/McDonnell Aircraft Company/U.S. Air Force Wright Aeronautical Laboratory investigated the effects of reverse thrust on the low-speed aerodynamics of an F-15 configuration. The F-15 model was fitted with a rotating van thrust reverser concept which could simulate both in-flight reversing for approach and landing or full reversing for ground roll reduction. The significant results of these two joint programs are reported. Banks, D. W. and Quinto, P. F. and Paulson, J. W., Jr. Langley Research Center NASA-TM-83277, NAS 1.15:83277 RTOP 505-42-23-01
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