A novel triaxial vibration test techniqueThe present work examines the circumstances under which simultaneous multiaxial vibration testing may be desirable, the testing techniques and equipment required to make it feasible, and the type of results that may be obtained together with some practical limitations to the techniques. Two schemes for performing vibration testing simultaneously or sequentially along three mutually perpendicular axes are considered and the most promising, involving a 'floating' technique, is presented in some detail. Practical problems associated with jig design and system resonances, cross-coupling between the various degrees of freedom, secondary loads on shaker elements, and system drift, are considered and workable solutions proposed. A simple simulation of multiaxial testing of a 1.1-pound inertia-simulated model of an Apollo command module is presented.
Document ID
19740059633
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Wignot, J. E. (Lockheed-California Co., Flutter and Aerodynamics Dept., Burbank Calif., United States)
Date Acquired
August 7, 2013
Publication Date
January 1, 1973
Subject Category
Facilities, Research, And Support
Meeting Information
Meeting: International Symposium on Space Technology and Science