Static and free-vibrational response of semi-circular graphite-epoxy frames with thin-walled open sections
By: J. Scott Collins, Eric R. Johnson.
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.
Series: [NASA contractor report] -- NASA CR-186097.; Interim report (NASA-Virginia Tech. Composites Program) -- 78.
Publisher: College of Engineering, Virginia Polytechnic Institute and State University
Published: 1989
Place of publication: Blacksburg, Va
Language: eng
Format: Microform
Number of pages: 204
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 titles: Static and free vibrational response of semi-circular graphite-epoxy frames with thin-walled open sections.
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."

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.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1990]. 3 microfiches : negative.

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