Research Catalog

Details

Additional authors

1. United States. National Aeronautics and Space Administration. Scientific and Technical Information Program, issuing body.

Description

1. 1 online resource (v, 30 pages) : illustrations.

Series statement

1. NASA technical memorandum ; 4770

Uniform title

1. NASA technical memorandum ; 4770.

Subject

1. Hypersonic aircraft
2. Finite element method
3. Mechanical properties
4. Thermal buckling
5. Aircraft structures

Call number

1. GPO Internet NAS 1.15:4770

Note

1. Title from title screen (viewed March 2, 2016).
2. "December 1996."

Bibliography (note)

1. Includes bibliographical references (page 15).

Author

1. Ko, William L., author.

Title

1. Thermal and mechanical buckling analysis of hypersonic aircraft hat-stiffened panels with varying face sheet geometry and fiber orientation / William L. Ko.

Publisher

1. [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, December 1996.

Type of content

1. text

Type of medium

1. computer

Type of carrier

1. online resource

Series

1. NASA technical memorandum ; 4770
2. NASA technical memorandum ; 4770.

Bibliography

1. Includes bibliographical references (page 15).

Connect to:

1. https://purl.fdlp.gov/GPO/gpo65666

Added author

1. United States. National Aeronautics and Space Administration. Scientific and Technical Information Program, issuing body.

Other form:

1. Print version: Ko, William L. Thermal and mechanical buckling analysis of hypersonic aircraft hat-stiffened panels with varying face sheet geometry and fiber orientation (OCoLC)36171323
2. Microfiche version: Ko, William L. Thermal and mechanical buckling analysis of hypersonic aircraft hat-stiffened panels with varying face sheet geometry and fiber orientation (OCoLC)37958339

Gpo item no.

1. 0830-D (online)

Sudoc no.

1. NAS 1.15:4770