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PRSEUS Pressure Cube Test Data and ResponseNASA s Environmentally Responsible Aviation (ERA) Program is examining the hybrid wing body (HWB) aircraft, among others, in an effort to increase the fuel efficiency of commercial aircraft. The HWB design combines features of a flying wing with features of conventional transport aircraft, and has the advantage of simultaneously increasing both fuel efficiency and payload. Recent years have seen an increased focus on the structural performance of the HWB. The key structural challenge of a HWB airframe is the ability to create a cost and weight efficient, non-circular, pressurized shell. Conventional round fuselage sections react cabin pressure by hoop tension. However, the structural configuration of the HWB subjects the majority of the structural panels to bi-axial, in-plane loads in addition to the internal cabin pressure, which requires more thorough examination and analysis than conventional transport aircraft components having traditional and less complex load paths. To address this issue, while keeping structural weights low, extensive use of advanced composite materials is made. This report presents the test data and preliminary conclusions for a pressurized cube test article that utilizes Boeing's Pultruded Rod Stitched Efficient Unitized Structure (PRSEUS), and which is part of the building block approach used for HWB development.
Document ID
20130013479
Acquisition Source
Langley Research Center
Document Type
Other
Authors
Lovejoy, Andrew E. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 27, 2013
Publication Date
May 1, 2013
Subject Category
Structural Mechanics
Report/Patent Number
L-20212
Funding Number(s)
WBS: WBS 699959.02.22.07.01.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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