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Rotary-wing aeroelasticity with application to VTOL vehiclesA concise assessment is presented of the state of the art in the field of rotary-wing aeroelasticity (RWE). The basic ingredients of RWE are reviewed, including structural modeling, unsteady aerodynamic modeling, formulation of the equations of motion, and solution methods. Results illustrating these methods are presented for isolated blades and coupled rotor-fuselage problems. The application of active controls to suppress aeromechanical and aeroelastic instabilities and to reduce vibration in rotorcraft is discussed. Structural optimization with aeroelastic constraints, gust response analysis of helicopters, and aeroelastic problems in special VTOL vehicles are briefly examined.
Document ID
19940036041
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Friedmann, Peretz P.
(California Univ. Los Angeles, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1993
Publication Information
Publication: In: Flight-vehicle materials, structures, and dynamics - Assessment and future directions. Vol. 5 - Structural dynamics and aeroelasticity (A94-12676 02-39)
Publisher: American Society of Mechanical Engineers
Subject Category
Aircraft Stability And Control
Accession Number
94A12696
Funding Number(s)
CONTRACT_GRANT: DAAL03-88-C-0003
CONTRACT_GRANT: NAG1-833
CONTRACT_GRANT: NAG2-477
CONTRACT_GRANT: DAAL03-89-K-0007
Distribution Limits
Public
Copyright
Other

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