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Utilization of the Building-Block Approach in Structural Mechanics ResearchIn the last 20 years NASA has worked in collaboration with industry to develop enabling technologies needed to make aircraft safer and more affordable, extend their lifetime, improve their reliability, better understand their behavior, and reduce their weight. To support these efforts, research programs starting with ideas and culminating in full-scale structural testing were conducted at the NASA Langley Research Center. Each program contained development efforts that (a) started with selecting the material system and manufacturing approach; (b) moved on to experimentation and analysis of small samples to characterize the system and quantify behavior in the presence of defects like damage and imperfections; (c) progressed on to examining larger structures to examine buckling behavior, combined loadings, and built-up structures; and (d) finally moved to complicated subcomponents and full-scale components. Each step along the way was supported by detailed analysis, including tool development, to prove that the behavior of these structures was well-understood and predictable. This approach for developing technology became known as the "building-block" approach. In the Advanced Composites Technology Program and the High Speed Research Program the building-block approach was used to develop a true understanding of the response of the structures involved through experimentation and analysis. The philosophy that if the structural response couldn't be accurately predicted, it wasn't really understood, was critical to the progression of these programs. To this end, analytical techniques including closed-form and finite elements were employed and experimentation used to verify assumptions at each step along the way. This paper presents a discussion of the utilization of the building-block approach described previously in structural mechanics research and development programs at NASA Langley Research Center. Specific examples that illustrate the use of this approach are included from recent research and development programs for both subsonic and supersonic transports.
Document ID
20050199405
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Rouse, Marshall
(NASA Langley Research Center Hampton, VA, United States)
Jegley, Dawn C.
(NASA Langley Research Center Hampton, VA, United States)
McGowan, David M.
(NASA Langley Research Center Hampton, VA, United States)
Bush, Harold G.
(NASA Langley Research Center Hampton, VA, United States)
Waters, W. Allen
(Lockheed Martin Corp. Hampton, VA, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2005
Subject Category
Aircraft Design, Testing And Performance
Meeting Information
Meeting: 46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
Location: Austin, TX
Country: United States
Start Date: April 18, 2005
End Date: April 21, 2005
Sponsors: American Society of Mechanical Engineers, American Inst. of Aeronautics and Astronautics, Alpha STAR Corp., American Helicopter Society, Inc., American Society of Civil Engineers
Funding Number(s)
OTHER: 23-719-55-TA
Distribution Limits
Public
Copyright
Public Use Permitted.
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