Application of fiber bridging models to fatigue crack growth in unidirectional titanium matrix composites
By: J.G. Bakuckas, Jr. and W. S. Johnson.
Contributors: Johnson, W. S.; United States. National Aeronautics and Space Administration.
Series: NASA technical memorandum -- 107588.; NASA technical memorandum -- 107588.
Publisher: National Aeronautics and Space Administration; For sale by the National Technical Information Service
Published: 1992
Place of publication: [Washington, DC; Springfield, Va
Language: eng
Format: Microform
Subjects: Metallic composites -- Fatigue.; Titanium.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 93-0253-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration], 1992. 1 microfiche.