NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Test and Analysis of a Hyper-X Carbon-Carbon Leading Edge ChineDuring parts production for the X43A Mach 10 hypersonic vehicle nondestructive evaluation (NDE) of a leading edge chine detected on imbedded delamination near the lower surface of the part. An ultimate proof test was conducted to verify the ultimate strength of this leading edge chine part. The ultimate proof test setup used a pressure bladder design to impose a uniform distributed pressure field over the bi-planar surface of the chine test article. A detailed description of the chine test article and experimental test setup is presented. Analysis results from a linear status model of the test article are also presented and discussed. Post-test inspection of the specimen revealed no visible failures or areas of delamination.
Document ID
20050186551
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Smith, Russell W.
(NASA Langley Research Center Hampton, VA, United States)
Sikora, Joseph G.
(NASA Langley Research Center Hampton, VA, United States)
Lindell, Michael C.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 7, 2013
Publication Date
May 1, 2005
Subject Category
Air Transportation And Safety
Report/Patent Number
NASA/TM-2005-213765
L-19133
Funding Number(s)
WORK_UNIT: WU 23-376-70-30-04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available