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Damage Arresting Composites for Shaped Vehicles - Phase II Final ReportThis 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. In addition to the analytical studies, a three specimen test program was also completed to assess the concept under axial tension loading, axial compression loading, and internal pressure loading.
Document ID
20110004279
Acquisition Source
Langley Research Center
Document Type
Contractor Report (CR)
Authors
Velicki, Alex (Boeing Phantom Works Huntington Beach, CA, United States)
Yovanof, Nicolette (Boeing Phantom Works Huntington Beach, CA, United States)
Baraja, Jaime (Boeing Phantom Works Huntington Beach, CA, United States)
Linton, Kim (Boeing Phantom Works Huntington Beach, CA, United States)
Li, Victor (Boeing Phantom Works Huntington Beach, CA, United States)
Hawley, Arthur (Boeing Phantom Works Huntington Beach, CA, United States)
Thrash, Patrick (Boeing Phantom Works Huntington Beach, CA, United States)
DeCoux, Steve (Boeing Phantom Works Huntington Beach, CA, United States)
Pickell, Robert (Boeing Phantom Works Huntington Beach, CA, United States)
Date Acquired
August 25, 2013
Publication Date
January 1, 2011
Subject Category
Structural Mechanics
Report/Patent Number
NASA/CR-2011-216880
NF1676L-11864
Funding Number(s)
CONTRACT_GRANT: NNL07AA48C
WBS: WBS 699959.02.08.07.02.02
Distribution Limits
Public
Copyright
Public Use Permitted.

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