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Aerodynamics In Ground Effect And Predicted Landing Ground Roll Of A Fighter Configuration With A Secondary Nozzle Thrust Reverser
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Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781722928858 Total Pages :132 pages Book Rating :4.9/5 (288 download)
Book Synopsis Aerodynamics in Ground Effect and Predicted Landing Ground Roll of a Fighter Configuration with a Secondary-Nozzle Thrust Reverser by : National Aeronautics and Space Administration (NASA)
Download or read book Aerodynamics in Ground Effect and Predicted Landing Ground Roll of a Fighter Configuration with a Secondary-Nozzle Thrust Reverser 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 132 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental investigation of the in-ground effect aerodynamic characteristics and predicted landing-ground-roll performance of wing-canard fighter configuration with a secondary nozzle thrust reverser was completed. These tests were conducted in the Langley 14 by 22 foot Subsonic Wind Tunnel using a model equipped with a pneumatic jet for thrust simulation of nozzle pressure ratios up to 4.0. The model was tested in the landing rollout configuration at approx. wheel touchdown height for a range of decreasing dynamic pressure from 50 psf down to 10 psf. Landing-ground-roll predictions of the configuration were calculated using the wind tunnel results. Banks, Daniel W. Langley Research Center CASCADE FLOW; GROUND EFFECT (AERODYNAMICS); NOZZLE FLOW; ROLL; SHORT TAKEOFF AIRCRAFT; THRUST REVERSAL; AERODYNAMIC CONFIGURATIONS; AIRCRAFT CONFIGURATIONS; AIRCRAFT LANDING; CANARD CONFIGURATIONS; JET THRUST; PRESSURE RATIO; WIND TUNNEL TESTS...
Book Synopsis Aerodynamics in Ground Effect and Predicted Landing Ground Roll of a Fighter Configuration with a Secondary-nozzle Thrust Reverser by : Daniel W. Banks
Download or read book Aerodynamics in Ground Effect and Predicted Landing Ground Roll of a Fighter Configuration with a Secondary-nozzle Thrust Reverser written by Daniel W. Banks and published by . This book was released on 1988 with total page 136 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Investigation of the Aerodynamics in Ground Effect and Predicated Landing Ground Roll of a Fighter Configuartion with a Secondary-nozzle Thrust Reverser by : Daniel W. Banks
Download or read book An Investigation of the Aerodynamics in Ground Effect and Predicated Landing Ground Roll of a Fighter Configuartion with a Secondary-nozzle Thrust Reverser written by Daniel W. Banks and published by . This book was released on 1987 with total page 284 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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Book Synopsis Thrust-induced Effects on Low-speed Aerodynamics of Fighter Aircraft by :
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Book Synopsis Vectored Propulsion, Supermaneuverability and Robot Aircraft by : Benjamin Gal-Or
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Book Synopsis NASA Scientific and Technical Publications by : United States. National Aeronautics and Space Administration
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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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