Comprehensive structural dynamic analysis of the SSME/AT fuel pump first-stage turbine blade /

Bibliographic Details

Main Author:	Brown, A. M. (Author)
Format:	Government Document eBook
Language:	English
Published:	Marshall Space Flight Center, Alabama : National Aeronautics and Space Administration, Marshall Space Flight Center, August 1998.
Series:	NASA technical memorandum ; 1998-208594.
Subjects:	Dynamic structural analysis. Turbine blades. High pressure. Turbomachinery. Crack initiation. Evaluation. Displacement. Stresses and Loads
Online Access:	https://purl.fdlp.gov/GPO/gpo83498