NDLI: Damage arresting composites for shaped vehicles

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Damage arresting composites for shaped vehicles

Content Provider	NASA Technical Reports Server (NTRS)
Author	Velicki, Alex
Copyright Year	2009
Description	This report describes the development of a novel structural solution that addresses the demanding fuselage loading requirements for the Hybrid Wing or Blended Wing Body configurations that are described in NASA NRA subtopic A2A.3, "Materials and Structures for Wing Components and Non-Circular Fuselage." The phase I portion of this task includes a comprehensive finite element model-based structural sizing exercise performed using the BWB airplane configuration to generate internal loads and fuselage panel weights for an advanced Pultruded Rod Stitched Efficient Unitized Structure (PRSEUS) structural concept. An accompanying element-level test program is also described which substantiates the analytical results and calculation methods used in the trade study. The phase II plan for the continuation of this research is also included herein.
File Size	37737218
Page Count	97
File Format	PDF
Alternate Webpage(s)	http://archive.org/details/NASA_NTRS_Archive_20090034167
Archival Resource Key	ark:/13960/t80k7c17w
Language	English
Publisher Date	2009-09-01
Access Restriction	Open
Subject Keyword	Structural Mechanics Wings Aerodynamic Configurations Blended-wing-body Configurations Fuselages Rods Damage Loads Forces Pultrusion Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science
Content Type	Text
Resource Type	Technical Report

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