An investigation into the probabilistic combination of quasi-static and random accelerationsThe development of design load factors for aerospace and aircraft components and experiment support structures, which are subject to a simultaneous vehicle dynamic vibration (quasi-static) and acoustically generated random vibration, require the selection of a combination methodology. Typically, the procedure is to define the quasi-static and the random generated response separately, and arithmetically add or root sum square to get combined accelerations. Since the combination of a probabilistic and a deterministic function yield a probabilistic function, a viable alternate approach would be to determine the characteristics of the combined acceleration probability density function and select an appropriate percentile level for the combined acceleration. The following paper develops this mechanism and provides graphical data to select combined accelerations for most popular percentile levels.
Document ID
19840048859
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Schock, R. W. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Tuell, L. P. (NASA Marshall Space Flight Center Huntsville, AL, United States)