Accession Number : ADP003668

Title :   Snap-Through of Initially Buckled Beams under Uniform Random Pressure,

Corporate Author : UNIVERSITY OF SOUTHERN CALIFORNIA LOS ANGELES DEPT OF CIVIL ENGINEERING

Personal Author(s) : Seide,P.

Report Date : 1984

Pagination or Media Count : 12

Abstract : Aircraft structural components such as engine air intake ducting and rear fuselage and empennage structures which are located in the vicinity of jet engine exhausts experience combined heating and random dynamic excitation which result from the acoustic or pseudoacoustic noise emitted by the jet efflux.

Descriptors :   *Structural mechanics, *Vibration, Sound pressure, Beams(Structural), Buckling, Fuselages, Aircraft engine ducts, Structural response, Jet engine noise, Dynamic response, Random vibration

Distribution Statement : APPROVED FOR PUBLIC RELEASE