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
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