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NASA NTRS · 20070031993

Calculation of Dynamic Loads Due to Random Vibration Environments in Rocket Engine Systems

Abstract

An important part of rocket engine design is the calculation of random dynamic loads resulting from internal engine "self-induced" sources. These loads are random in nature and can greatly influence the weight of many engine components. Several methodologies for calculating random loads are discussed and then compared to test results using a dynamic testbed consisting of a 60K thrust engine. The engine was tested in a free-free condition with known random force inputs from shakers attached to three locations near the main noise sources on the engine. Accelerations and strains were measured at several critical locations on the engines and then compared to the analytical results using two different random response methodologies.

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BibTeXRIS

Christensen, Eric R., Brown, Andrew M., Frady, Greg P.. 2007-01-01. Calculation of Dynamic Loads Due to Random Vibration Environments in Rocket Engine Systems. https://ntrs.nasa.gov/citations/20070031993

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