NASA NTRS · 19940000690
Computing Response Of A Structure To Random Transient Pressures
Abstract
Improved method of computing vibrational response of structure to transient random acoustic excitation at predominantly low frequencies devised, called "deterministic". Motivated by need to analyze more accurately vibro/acoustic responses of structures at spacecraft-launching facilities and determine whether need for reinforcement or redesign to withstand launch environment. Also used to study such phenomena as earthquake motions, ocean waves, aircraft pressure gusts, responses of bridges to winds, and effects to jet-engine noise on aircraft structures.
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Sepcenko, Valentin, Margasahayam, Ravi. 1994-12-01. Computing Response Of A Structure To Random Transient Pressures. https://ntrs.nasa.gov/citations/19940000690
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