Role of the Material Constitutive Model in Simulating the Reusable Launch Vehicle Thrust Cell Liner Response
Author:
Affiliation:
1. Research Assistant, Johns Hopkins Univ., Baltimore, MD 21218.
2. Retired; formerly, Professor, Tel-Aviv Univ., Ramat-Aviv 69978, Israel.
3. PhD, Professor, Univ. of Virginia, Charlottesville, VA 22904.
Publisher
American Society of Civil Engineers (ASCE)
Subject
Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering
Link
http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%290893-1321%282005%2918%3A1%2828%29
Reference15 articles.
1. Higher-order theory for functionally graded materials
2. Armstrong W. H. (1979). “Structural analysis of cylindrical thrust chambers.” NASA Contractor Rep. No. 159522 Washington D.C.
3. Armstrong W. H. and Brogren E. W. (1975). “Thrust chamber life prediction. Volume II—Plug nozzle centerbody and cylinder life analysis.” NASA Contractor Rep. No. 134822 Washington D.C.
4. Armstrong W. H. and Brogren E. W. (1976). ”3-dimesional thrust chamber life prediction.” NASA Contractor Rep. No. 134979 Washington D.C.
5. Arnold S. M. (1987). “Effects of state recovery on creep buckling induced by thermomechanical loading.” PhD dissertation Univ. of Akron Akron Ohio.
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