NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Advanced Durability and Damage Tolerance Design and Analysis Methods for Composite Structures: Lessons Learned from NASA Technology Development ProgramsAerospace vehicles are designed to be durable and damage tolerant. Durability is largely an economic life-cycle design consideration whereas damage tolerance directly addresses the structural airworthiness (safety) of the vehicle. However, both durability and damage tolerance design methodologies must address the deleterious effects of changes in material properties and the initiation and growth of microstructural damage that may occur during the service lifetime of the vehicle. Durability and damage tolerance design and certification requirements are addressed for commercial transport aircraft and NASA manned spacecraft systems. The state-of-the-art in advanced design and analysis methods is illustrated by discussing the results of several recently completed NASA technology development programs. These programs include the NASA Advanced Subsonic Technology Program demonstrating technologies for large transport aircraft and the X-33 hypersonic test vehicle demonstrating technologies for a single-stage-to-orbit space launch vehicle.
Document ID
20030059016
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Harris, Charles E.
(NASA Langley Research Center Hampton, VA, United States)
Starnes, James H., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Shuart, Mark J.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 7, 2013
Publication Date
June 1, 2003
Subject Category
Mechanical Engineering
Report/Patent Number
L-18297
NASA/TM-2003-212420
NAS 1.15:212420
Report Number: L-18297
Report Number: NASA/TM-2003-212420
Report Number: NAS 1.15:212420
Funding Number(s)
OTHER: 706-85-12-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available