Model verification and validation concepts for a probabilistic fracture assessment model to predict cracking of knife edge seals in the space shuttle main engine high pressure oxidizer /

Bibliographic Details

Main Authors:	Pai, Shantaram S. (Author), Riha, David S. (Author)
Corporate Authors:	United States. National Aeronautics and Space Administration (sponsoring body.), ASME Turbo Expo
Format:	Government Document Conference Proceeding eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2013]
Series:	NASA technical memorandum ; 217849.
Subjects:	Flutter. Cracking (fracturing) Prediction analysis techniques. Fracture mechanics. Probability theory. Proving. Fatigue life. Fatigue (materials) Mathematical models.
Online Access:	https://purl.fdlp.gov/GPO/gpo40538 http://purl.fdlp.gov/GPO/gpo40538