Cyclic Stress Analysis of a Rocket Engine Thrust Chamber Using Chaboche, Voce and Creep Constitutive Models
- 6 January 2016
- journal article
- Published by Springer Science and Business Media LLC in Transactions of the Indian Institute of Metals
- Vol. 69 (2), 495-500
- https://doi.org/10.1007/s12666-015-0799-y
Abstract
No abstract availableKeywords
This publication has 5 references indexed in Scilit:
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- Comparison of Creep Properties of Four Copper Alloys and Creep Based Stress Analysis of a Rocket Engine Combustion ChamberProcedia Engineering, 2013
- Low Cycle Fatigue Behaviour of a Cu-Cr-Zr-Ti AlloyProcedia Engineering, 2013
- Stress analysis & life prediction of a cryogenic rocket engine thrust chamber considering low cycle fatigue, creep and thermal ratchettingTransactions of the Indian Institute of Metals, 2010
- On some modifications of kinematic hardening to improve the description of ratchetting effectsInternational Journal of Plasticity, 1991