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Subscale Test Methods for Combustion DevicesStated goals for long-life LRE s have been between 100 and 500 cycles: 1) Inherent technical difficulty of accurately defining the transient and steady state thermochemical environments and structural response (strain); 2) Limited statistical basis on failure mechanisms and effects of design and operational variability; and 3) Very high test costs and budget-driven need to protect test hardware (aversion to test-to-failure). Ambitious goals will require development of new databases: a) Advanced materials, e.g., tailored composites with virtually unlimited property variations; b) Innovative functional designs to exploit full capabilities of advanced materials; and c) Different cycles/operations. Subscale testing is one way to address technical and budget challenges: 1) Prototype subscale combustors exposed to controlled simulated conditions; 2) Complementary to conventional laboratory specimen database development; 3) Instrumented with sensors to measure thermostructural response; and 4) Coupled with analysis
Document ID
20050217140
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Anderson, W. E.
(Purdue Univ. West Lafayette, IN, United States)
Sisco, J. C.
(Purdue Univ. West Lafayette, IN, United States)
Long, M. R.
(Purdue Univ. West Lafayette, IN, United States)
Sung, I.-K.
(Purdue Univ. West Lafayette, IN, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2005
Publication Information
Publication: Fifth International Symposium on Liquid Space Propulsion
Subject Category
Aeronautics (General)
Funding Number(s)
CONTRACT_GRANT: NAG8-1876
CONTRACT_GRANT: NAG8-1856
CONTRACT_GRANT: NAG8-1894
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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