Cryogenic Temperature Effects on Metal Mesh Dampers and Liquid Hydrogen Turbopump Rotordynamics
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American Institute of Aeronautics and Astronautics
Reference4 articles.
1. 1Zarzour, M., Vance, J.M. "Experimental Evaluation of a Metal Mesh Bearing Damper", ASMEJournal of Engineering for Gas Turbines and Power, April 2000.
2. The Space Shuttle Main Engine High-Pressure Fuel Turbopump Rotordynamic Instability Problem
3. 4Okayasu, A., Ohta, T., Azuma, T., Fujita, T., and Aoki, H. 1990 "Vibration Problems In The LE-7 Liquid Hydrogen Turbopump", Proceedings of the 26thAIAA Joint Propulsion Conference, pp.1-5.
4. 5Ertas, B.H., Vance, J.M. "The Effect of Static and Dynamic Misalignment on Ball Bearing Radial Stiffness," 38thAIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, July 7th- July 10th2002, Paper # 4160.
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