Effect of rim thickness on gear crack propagation path
By: David G. Lewicki and Roberto Ballarini.
Contributors: Ballarini, Roberto.; United States. National Aeronautics and Space Administration.; U.S. Army Research Laboratory.
Series: NASA technical memorandum -- 107229.; Army research laboratory technical report -- ARL-TR-1110.
Publisher: National Aeronautics and Space Administration; U.S. Army Research Laboratory; National Technical Information Service, distributor
Published: 1996
Place of publication: [Washington, DC; Springfield, Va
Language: eng
Format: Microform
Subjects: Gears.; Crack propagation.; Gear teeth.; Bending fatigue.; Fatigue tests.; Finite element method.; Computerized simulation.
Notes: Shipping list no.: 98-0769-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1997] 1 microfiche.