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Static and free-vibrational response of semi-circular graphite-epoxy frames with thin-walled open sections /

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Bibliographic Details
Main Author: Collins, J. Scott
Corporate Authors: NASA-Virginia Tech. Composites Program, Virginia Polytechnic Institute and State University. Center for Composite Materials and Structures, Langley Research Center. Landing and Impact Dynamics Branch
Other Authors: Johnson, Eric R.
Format: Government Document Microform Book
Language:English
Published: Blacksburg, Va. : College of Engineering, Virginia Polytechnic Institute and State University, [1989]
Series:Interim report (NASA-Virginia Tech. Composites Program) ; 78.
NASA contractor report ; NASA CR-186097.
Subjects:
Fibrous composites > Testing.
Fibrous composites > Vibration.
Airframes > Testing.
Graphite fibers.
Epoxy resins.
Composite structures.
Dynamic tests.
Free vibration.
Graphite-epoxy composites.
Load tests.
Static tests.
Structural vibration.
Vibration tests.
Online Access:https://purl.fdlp.gov/GPO/LPS69421
Description
Item Description:"CCMS-89-21."
"VPI-E-89-19."
"October 1989."
Department of Aerospace Engineering."."
"Virginia Tech Center for Composite Materials and Structures"--Cover.
Shipping list number: 90-0857-M.
Microform.
Physical Description:xii, 204 pages : illustrations ; 28 cm.
Also available via Internet from the NASA Technical Report Server web site. Address as of 5/3/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900004284%5F1990004284.pdf; current access available via PURL.
Bibliography:Includes bibliographical references (pages 166-168).