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An optimization approach to vibration reduction in helicopter rotors with multiple active trailing edge flaps

  • Published:2004-04 Issue:3 Volume:8 Page:185-194
  • ISSN:1270-9638
  • Container-title:Aerospace Science and Technology
  • language:en
  • Short-container-title:Aerospace Science and Technology

Author:

Viswamurthy Sathyamangalam Ramanarayanan,Ganguli Ranjan

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference29 articles.

1. Theory of Wing Sections;Abbott,1959

2. G. Bir, et al., Univeristy of Maryland Advanced Rotorcraft Code (UMARC) Theory Manual, UM-AERO Report 92-02, 1992

3. Induced-shear piezoelectric actuators for rotor blade trailing edge flaps;Centolanza;Smart Materials and Structures,2002

4. Status of application of smart structures technology to rotorcraft systems;Chopra;J. Amer. Helicopter Soc.,2000

5. Review of state of art of smart structures and integrated sytems;Chopra;AIAA J.,2002

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