Residual strength of five boron/aluminum laminates with crack-like notches after fatigue loading
By: R.A. Simonds ; prepared for Langley Research Center.
Contributors: Langley Research Center.; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.; Virginia Polytechnic Institute and State University.
Series: NASA contractor report -- 3815.; NASA contractor report -- NASA CR-3815.
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch; For sale by the National Technical Information Service]
Published: 1984
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Number of pages: 35
Subjects: Aluminum -- Fatigue.; Boron.; Metals -- Fatigue.
Notes: "Virginia Polytechnic Institute and State University."

Distributed to depository libraries in microfiche.

"July 1984"--Cover.

Subject category 24.

Includes bibliographical references.

Final report-task 3.

NAS1-17100.