Snap-Through of Initially Buckled Beams under Uniform Random Pressure,
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.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jan 01, 1984
- Accession Number
- ADP003668
Entities
People
- P. Seide
Organizations
- University of Southern California