NASA Technical Reports Server (NTRS) 19730010070: Study of inducer load and stress, volume 2Report as inadecuate




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A program of analysis, design, fabrication and testing has been conducted to develop computer programs for predicting rocket engine turbopump inducer hydrodynamic loading, stress magnitude and distribution, and vibration characteristics. Methods of predicting blade loading, stress, and vibration characteristics were selected from a literature searc

Author: NASA Technical Reports Server (NTRS)

Source: https://archive.org/







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