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Static and free-vibrational response of semi-circular graphite-epoxy frames with thin-walled open sections [microform] / J. Scott Collins, Eric R. Johnson
Bib ID 4036381
Format BookBook, MicroformMicroform, OnlineOnline
Author
Collins, J. Scott
 
Online Versions
Description Blacksburg, Va. : College of Engineering, Virginia Polytechnic Institute and State University, [1989] 
xii, 204 p. : ill. ; 28 cm. 
Series

[NASA contractor report] ; NASA CR-186097.

Interim report (NASA-Virginia Tech. Composites Program) ; 78.

Notes

Department of Aerospace Engineering."

"Virginia Tech Center for Composite Materials and Structures"--Cover.

Shipping list no.: 90-0857-M.

"October 1989."

"CCMS-89-21."

"VPI-E-89-19."

Distributed to depository libraries on microfiche.

Includes bibliographical references (p. 166-168).

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.

Prepared for Landing and Impact Dynamics Branch, National Aeronautics and Space Administration, Langley Research Center NAG-1-343

Reproduction Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1990]. 3 microfiches : negative. 
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.
Other authors/contributors Johnson, Eric R  |  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
Also Titled

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

Available From NASA 
Govt. Doc. Number NAS 1.26:186097 

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