Structural design optimization of a tiltrotor aircraft composite wing to enhance whirl flutter stability

Author:

Kim Taeseong,Lim Jaehoon,Shin SangJoon,Kim Do-Hyung

Publisher

Elsevier BV

Subject

Civil and Structural Engineering,Ceramics and Composites

Reference35 articles.

1. Prop-rotor stability at high advance ratios;Hall;J Am Helicopter Soc,1966

2. Acree Jr CW, Peyran RJ, Johnson W. Rotor design options for improving XV-15 whirl-flutter stability margins. NASA Technical paper-2004-212262; March, 2004.

3. Acree Jr CW, Peyran Jr RJ, Johnson W. Rotor design for whirl flutter: an examination of options for improving tiltrotor aeroelastic stability margins. In: American helicopter society 55th international annual forum proceedings, Alexandria, VA; May 25–27, 1999.

4. Acree Jr CW. Effects of rotor design variations on tiltrotor whirl mode stability. In: Tiltrotor/runway independent aircraft technology and applications specialists’ meeting, Arlington, Texas; March 20–21, 2001.

5. Acree Jr CW. Rotor design options for improving V-22 whirl mode stability. In: American helicopter society 58th international annual forum proceedings, Montréal, Quebec, Canada; June 11–13, 2002.

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