Research Catalog

Title

Nonlinear response and residual strength of damaged stiffened shells subjected to combined loads [microform] / James H. Starnes, Jr. ... [et al.].

Publication

[Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]

Details

Additional Authors

• Starnes, James H.
• United States. National Aeronautics and Space Administration.

Description

1 v.

Series Statement

NASA-TM ; 111889

Uniform Title

NASA technical memorandum ; 111889.

Subject

• Crack propagation
• Stress intensity factors
• Fuselages
• Shells (Structural forms)
• Residual strength
• Reinforced shells
• Stress distribution
• Finite element method
• Structural analysis

Note

• Shipping list no.: 97-0681-M.

Reproduction (note)

• Microfiche.

Call Number

READEX Microfiche NAS 1.15:111889

OCLC

marcive42787290

Title

Nonlinear response and residual strength of damaged stiffened shells subjected to combined loads [microform] / James H. Starnes, Jr. ... [et al.].

Imprint

[Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]

Series

NASA-TM ; 111889

NASA technical memorandum ; 111889.

Reproduction

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1997] 1 microfiche.

Added Author

Starnes, James H.

United States. National Aeronautics and Space Administration.

Gpo Item No.

0830-D (MF)

Sudoc No.

NAS 1.15:111889

Research Call Number

READEX Microfiche NAS 1.15:111889