Comparison of Creep Properties of Four Copper Alloys and Creep Based Stress Analysis of a Rocket Engine Combustion Chamber-Reference-Cited by-同舟云学术

Comparison of Creep Properties of Four Copper Alloys and Creep Based Stress Analysis of a Rocket Engine Combustion Chamber

Published:2013 Issue: Volume:55 Page:45-50
ISSN:1877-7058
Container-title:Procedia Engineering
language:en
Short-container-title:Procedia Engineering

Author:

Asraff A.K.,Aparna R.,Kumaresan D.,Muthukumar R.

Publisher

Elsevier BV

Subject

Applied Mathematics

Reference4 articles.

1. Anonymous, ANSYS- Engineering analysis system, Users Manual. ANSYS Inc, USA, (2009).

2. David L. Ellis & Gary M. Michal, Mechanical and Thermal Properties of two Cu-Cr-Nb alloys and NARloy-Z, NASA CR 198529, (1996), National Aeronautical & Space Administration, USA.

3. A.K. Asraff, S. Sunil, R. Muthukumar, T.J. Ramanathan, Stress analysis and life prediction of a rocket engine thrust chamber considering low cycle fatigue, creep and thermal ratcheting, Transactions of the Indian Institute of Metals, Vol. 63, (2010), pp 601-606.

4. Aparna, Creep modelling and stress analysis of a double walled cryogenic rocket thrust chamber, M. Tech dissertation, Mahatma Gandhi University, Kerala, 2011.

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