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Aircraft aeroelasticity and structural dynamics research at the NASA Langley Research Center - Some illustrative resultsHighlights of nine different research studies are described. Five of these topics relate directly to fixed-wing aircraft and range from flutter studies using relatively simple and inexpensive wind-tunnel models to buffet studies of the vertical tails of an advanced high-performance configuration. The other four topics relate directly to rotary-wing aircraft and range from studies of the performance and vibration characteristics of an advanced rotor design to optimization of airframe structures for vibration attenuation.
Document ID
19890026239
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Doggett, Robert V., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Cazier, F. W., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1988
Subject Category
Aircraft Design, Testing And Performance
Meeting Information
Meeting: ICAS Congress
Location: Jerusalem
Country: Israel
Start Date: August 28, 1988
Sponsors: ICAS
Accession Number
89A13610
Distribution Limits
Public
Copyright
Other

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