A comparison of fatigue life prediction methodologies for rotor craft
By: R.A. Everett, Jr.
Contributors: United States. Army Aviation Research and Technology Activity.; Langley Research Center.
Series: NASA technical memorandum -- 102759.; AVSCOM technical report -- 90-B-011.; AVSCOM technical report -- 90-B-11.
Publisher: National Aeronautics and Space Administration, Langley Research Center; US Army Aviation Systems Command, Aviation R&T Activity; National Technical Information Service, distributor
Published: 1990
Place of publication: Hampton, Va; [St. Louis, Mo.]; [Springfield, Va
Language: eng
Format: Microform
Subjects: Crack propogation.; Fatigue life.; Notch tests.; Palmgren-Miner rule.; Probability theory.; Prediction analysis techniques.; Reliability analysis.; Rotary wing aircraft.
Notes: Distributed to depository libraries in microfiche.

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