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Publisher: IOP Publishing

Volume 10, Number 1, 2001

Wind tunnel testing of a Mach-scaled rotor model with trailing-edge flaps
pp. 1-14(14)
Authors: Koratkar, N.A.; Chopra, I.

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Development of a piezoelectric actuator for trailing edge flap control of full scale rotor blades
pp. 25-34(10)
Authors: Straub, F.K.; Ngo, H.T.; Anand, V.; Domzalski, D.B.

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On the twist performance of a multiple-cell active helicopter blade
pp. 53-61(9)
Authors: Cesnik, C.E.S.; Shin, S.

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Dynamic response of active twist rotor blades
pp. 62-76(15)
Authors: Cesnik, C.E.S.; Shin, S.; Wilbur, M.L.

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Blade-vortex interaction noise reduction with active twist smart rotor technology
pp. 77-85(9)
Authors: Chen, P.C.; Baeder, J.D.; Evans, R.A.D.; Niemczuk, J.

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Analytical study of active control of wave transmission through cylindrical struts
pp. 121-136(16)
Authors: Pelinescu, I.; Balachandran, B.

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On the role of prediction tools for adaptive rotor system developments
pp. 137-144(8)
Authors: Kube, R.; Klppel, V.

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Classifying helicopter gearbox faults using a normalized energy metric
pp. 145-153(9)
Authors: Samuel, P.D.; Pines, D.J.

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