NASA Technical Reports Server (NTRS) 19730010070: Study of inducer load and stress, volume 2Reportar como inadecuado




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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

Autor: NASA Technical Reports Server (NTRS)

Fuente: https://archive.org/







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