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Record 1 of 48490
Flight-vehicle materials, structures, and dynamics - Assessment and future directions. Vol. 5 - Structural dynamics and aeroelasticity
Author and Affiliation:
Noor, Ahmed K. [Editor](Virginia Univ., NASA, Langley Research Center)
Venneri, Samuel L. [Editor](NASA Washington, United States)
Abstract: Various 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.
Publication Date: Jan 01, 1993
Document ID:
19940036021
(Acquired Dec 28, 1995)
Accession Number: 94A12676
Subject Category: STRUCTURAL MECHANICS
ISBN: ISBN 0-7918-0663-4
Document Type: Collected Works
Publication Information: 521 p.; (SEE A94-12677 through A94-12698)
Publisher Information: American Society of Mechanical Engineers, New York, United States
Organization Source: NASA Langley Research Center; Hampton, VA, United States
NASA; Washington, DC, United States
Description: 521p; In English
Distribution Limits: Unclassified; Publicly available; Unlimited
Rights: Copyright
NASA Terms: AEROELASTICITY; AIRCRAFT STRUCTURES; DYNAMIC STRUCTURAL ANALYSIS; AEROACOUSTICS; AEROELASTIC RESEARCH WINGS; AEROSERVOELASTICITY; CONTROL EQUIPMENT; DYNAMIC TESTS; ELASTODYNAMICS; MATHEMATICAL MODELS; ROTATING BODIES; STRUCTURAL DESIGN; SYSTEM IDENTIFICATION; VIBRATION DAMPING; VIBRATION TESTS; WIND TUNNEL TESTS
Miscellaneous Notes: For individual items see A94-12677 to A94-12698
Availability Source: Other Sources
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