Space Shuttle Main Engine Powerhead Structural Modeling, Stress and Fatigue Life Analysis. Volume 2: Dynamics of Blades and Nozzles SSME HPFTP and HPOTP

摘要

Normal modes of the blades and nozzles of the HPFTP and HPOTP are defined and potential driving forces for the blades are identified. The computer models used in blade analyses are described, with results. Similar information is given for the nozzles.