Effect of initial delamination on mode I and mode II interlaminar fracture toughness and fatigue fracture threshold
By: Gretchen Bostaph Murri and Roderick H. Martin.
Contributors: Martin, Roderick H.; United States. Army Aviation Research and Technology Activity.; Langley Research Center.
Series: NASA technical memorandum -- 104079.; AVSCOM TR -- 91-B-005.; AVSCOM technical report -- 91-B-5.
Publisher: National Aeronautics and Space Administration, Langley Research Center
Published: 1991
Place of publication: Hampton, Va
Language: eng
Format: Microform
Subjects: Composite materials -- Delamination.; Strength of materials.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 92-096-M.

Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration], 1991. 1 microfiche.