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Active Load Control During Rolling Maneuvers Performed In The Langley Transonic Dynamics Tunnel
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Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781722156879 Total Pages :64 pages Book Rating :4.1/5 (568 download)
Book Synopsis Active Load Control During Rolling Maneuvers. Performed in the Langley Transonic Dynamics Tunnel by : National Aeronautics and Space Administration (NASA)
Download or read book Active Load Control During Rolling Maneuvers. Performed in the Langley Transonic Dynamics Tunnel written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-06 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt: A rolling maneuver load alleviation (RMLA) system has been demonstrated on the active flexible wing (AFW) wind tunnel model in the Langley Transonic Dynamics Tunnel (TDT). The objective was to develop a systematic approach for designing active control laws to alleviate wing loads during rolling maneuvers. Two RMLA control laws were developed that utilized outboard control-surface pairs (leading and trailing edge) to counteract the loads and that used inboard trailing-edge control-surface pairs to maintain roll performance. Rolling maneuver load tests were performed in the TDT at several dynamic pressures that included two below and one 11 percent above open-loop flutter dynamic pressure. The RMLA system was operated simultaneously with an active flutter suppression system above open-loop flutter dynamic pressure. At all dynamic pressures for which baseline results were obtained, torsion-moment loads were reduced for both RMLA control laws. Results for bending-moment load reductions were mixed; however, design equations developed in this study provided conservative estimates of load reduction in all cases. Woods-Vedeler, Jessica A. and Pototzky, Anthony S. and Hoadley, Sherwood T. Langley Research Center...
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