Skin/stiffener interface stresses in composite stiffened panels
By: J.T.S. Wang, S.B. Biggers.
Contributors: Biggers, Sherrill B.; Lockheed-Georgia Company.; Langley Research Center.
Series: NASA contractor report -- 172261.; NASA contractor report -- NASA CR-172261.
Publisher: Lockheed-Georgia Company; National Aeronautics and Space Administration, Langley Research Center
Published: 1984
Place of publication: Marietta, Ga; Hampton, Va
Language: eng
Format: Microform
Subjects: Composite materials.; Buckling (Mechanics); Composite structures.; Interlayers.; Panels.; Skin (structural member); Stiffening.; Stress analysis.
Notes: Also available via Internet from the NTRS web site. Address as of 11/26/07: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19840010613%5F1984010613.pdf  ; current access is available via PURL.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration], 1984. 1 microfiche.