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Structural dynamic and aeroelastic considerations for hypersonic vehiclesThe specific geometrical, structural, and operational environment characteristics of hypersonic vehicles are discussed with particular reference to aerospace plane type configurations. A discussion of the structural dynamic and aeroelastic phenomena that must be addressed for this class of vehicles is presented. These phenomena are in the aeroservothermoelasticity technical area. Some illustrative examples of recent experimental and analytical work are given. Some examples of current research are pointed out.
Document ID
19910017819
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Cazier, F. W., Jr. (NASA Langley Research Center Hampton, VA, United States)
Doggett, Robert V., Jr. (NASA Langley Research Center Hampton, VA, United States)
Ricketts, Rodney H. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
June 1, 1991
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-104110
NAS 1.15:104110
Report Number: NASA-TM-104110
Report Number: NAS 1.15:104110
Meeting Information
Meeting: AIAA/ASME/ASCE/AHS/ASC 32d Structures, Structural Dynamics, and Materials Conference
Location: Baltimore, MD
Country: United States
Start Date: April 8, 1991
End Date: April 10, 1991
Accession Number
91N27133
Funding Number(s)
PROJECT: RTOP 763-23-41
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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