Browsing by Subject "Active Rotors"
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ItemA conceptual design of active tab for Mach scaled model blade installation( 2010) Noboru, K. ; Saito, S.
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ItemAn examination of the effect of trailing edge flaps on swashplateless rotor performance( 2010) Falls, J. ; Datta, A. ; Chopra, I.
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ItemBenefit studies for rotor with active twist control using weak fluid-structure coupling( 2009) Zhang, Q. ; Hoffmann, F. ; Wall, B.G. van der
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ItemDetermination of optimum camber distribution in rotating wings with deformable airfoils for vibration reduction and performance enhancement using surrogate modeling( 2010) Kumar, D. ; Glaz, B. ; Mok, J. ; Friedmann, P.P. ; Cesnik, C.E.S.
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ItemHelicopter blade twist control through sma technology: optimal shape prediction, twist actuator realisation and main rotor enhanced performance computation( 2009) Pagano, A. ; Ameduri, S. ; Cokonaj, V. ; Prachar, A. ; Zachariadis, Z. ; Drikakis, D.
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ItemHelicopter performance improvement with variable chord morphing rotors( 2010) Khoshlahjeh, M. ; Sung Bae, E. ; Gandhi, F.
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ItemImprovement of noise reduction and performance for a helicopter model rotor blade by active twist actuation( 2009) Bailly, J. ; Delrieux, Y.
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ItemNovel concept for realizing individual blade control (IBC) for helicopters( 2010) Bartels, R. ; Kueffmann, P. ; Kessler, Ch.
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ItemRotor power reduction using multiple spanwise-segmented, optimally-actuated trailing-edge flaps( 2009) Leon, O. ; Gandhi, F.
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ItemSmart rotor development and wind tunnel test( 2009) Straub, F.K. ; Anand, V.R. ; Birchette, T.S. ; Lau, B.H.
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ItemStructural design and testing of active twist blades - a comparison( 2009) Riemenschneider, J. ; Opitz, S. ; Wierach, P. ; Rochettes, H. Mercier Des ; Buchaniek, L. ; Joly, D.
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ItemVibration reduction in rotorcraft using active microflaps( 2010) Padthe, A. ; Liu, L. ; Friedmann, P.P.