buckling strength of filament-wound cylinders under axial compression
By: prepared under contract by Martin-Marietta Corporation for National Aeronautics and Space Administration.
Contributors: Feldman, A.; Stang, D. A.; Martin-Marietta Corporation; United States. National Aeronautics and Space Administration.
Publisher: NASA
Published: 1965
Place of publication: Washington
Number of pages: 58
Subjects: Axial compression loads; Buckling; Cylindrical shells; Filament winding
Notes: Bibliographical references: p.16-17.

Contract number: NASw-912