This report describes the development of a novel structural concept, Pultruded Rod Stitched Efficient Unitized Structure (PRSEUS), that addresses the demanding fuselage loading requirements for the Hybrid Wing or Blended Wing Body (BWB) airplane configuration with regards to acoustic response. A PRSEUS panel was designed and fabricated and provided to NASA-LaRC for acoustic response testing in the Structural Acoustics Loads and Transmission (SALT) facility. Preliminary assessments of the sound transmission characteristics of a PRSEUS panel subjected to a representative Hybrid Wing Body (HWB) operating environment were completed for the NASA Environmentally Responsible Aviation (ERA) Program.
PRSEUS Acoustic Panel Fabrication
2011
49 pages
Report
Keine Angabe
Englisch
PRSEUS Acoustic Panel Fabrication
NTRS | 2011
|PRSEUS Panel Fabrication Final Report
NTIS | 2014
|PRSEUS Panel Fabrication Final Report
NTRS | 2014
|PRSEUS Structural Concept Development
NTRS | 2014
|Pressure Testing of a Minimum Gauge PRSEUS Panel
British Library Conference Proceedings | 2011
|