Compression response of a sandwich fuselage keel panel with and without damage [microform] / David M. McGowan and Damodar R. Ambur.

Saved in:

Bibliographic Details
Main Author:	McGowan, David M.
Corporate Author:	Langley Research Center
Other Authors:	Ambur, Damodar R.
Format:	Government Document Microfilm Book
Language:	English
Published:	Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], [1997]
Series:	NASA technical memorandum ; 110302.
Subjects:	Superconducting composites. Airplanes > Fuselage. Composite structures. Finite element method. Fuselages. Graphite-epoxy composites. Honeycomb cores. Impact damage. Sandwich structures.

Norlin Library - Government Information - Microform

Holdings details from Norlin Library - Government Information - Microform
Call Number:	NAS 1.15:110302
NAS 1.15:110302	Restricted Place a Hold