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Ground Vibration And Flight Flutter Tests Of The Single Seat F 16xl Aircraft With A Modified Wing
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Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781722423865 Total Pages :64 pages Book Rating :4.4/5 (238 download)
Book Synopsis Ground Vibration and Flight Flutter Tests of the Single-Seat F-16xl Aircraft with a Modified Wing by : National Aeronautics and Space Administration (NASA)
Download or read book Ground Vibration and Flight Flutter Tests of the Single-Seat F-16xl Aircraft with a Modified Wing written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-08 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt: The NASA single-seat F-16XL aircraft was modified by the addition of a glove to the left wing. Vibration tests were conducted on the ground to assess the changes to the aircraft caused by the glove. Flight Luther testing was conducted on the aircraft with the glove installed to ensure that the flight envelope was free of aeroelastic or aeroservoelastic instabilities. The ground vibration tests showed that above 20 Hz, several modes that involved the control surfaces were significantly changed. Flight test data showed that modal damping levels and trends were satisfactory where obtainable. The data presented in this report include estimated modal parameters from the ground vibration and flight flutter test. Voracek, David F. Armstrong Flight Research Center...
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