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Flight-vehicle materials, structures, and dynamics - Assessment and future directions. Vol. 5 - Structural dynamics and aeroelasticityVarious papers on flight vehicle materials, structures, and dynamics are presented. Individual topics addressed include: general modeling methods, component modeling techniques, time-domain computational techniques, dynamics of articulated structures, structural dynamics in rotating systems, structural dynamics in rotorcraft, damping in structures, structural acoustics, structural design for control, structural modeling for control, control strategies for structures, system identification, overall assessment of needs and benefits in structural dynamics and controlled structures. Also discussed are: experimental aeroelasticity in wind tunnels, aeroservoelasticity, nonlinear aeroelasticity, aeroelasticity problems in turbomachines, rotary-wing aeroelasticity with application to VTOL vehicles, computational aeroelasticity, structural dynamic testing and instrumentation.
Document ID
19940036021
Acquisition Source
Legacy CDMS
Document Type
Other - Collected Works
Authors
Noor, Ahmed K.
(Virginia Univ.; NASA, Langley Research Center Hampton, United States)
Venneri, Samuel L.
(NASA Headquarters Washington, DC United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1993
Publication Information
Publisher: American Society of Mechanical Engineers
ISBN: 0-7918-0663-4
Subject Category
Structural Mechanics
Accession Number
94A12676
Distribution Limits
Public
Copyright
Other

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